id	sid	tid	token	lemma	pos
ap-8157	1	1	acta	acta	PROPN
ap-8157	1	2	polytechnica	polytechnica	PROPN
ap-8157	1	3	https://doi.org/10.14311/ap.2022.62.0549	https://doi.org/10.14311/ap.2022.62.0549	PROPN
ap-8157	1	4	acta	acta	PROPN
ap-8157	1	5	polytechnica	polytechnica	PROPN
ap-8157	1	6	62(5):549–557	62(5):549–557	PROPN
ap-8157	1	7	,	,	PUNCT
ap-8157	1	8	2022	2022	NUM
ap-8157	1	9	©	©	ADP
ap-8157	1	10	2022	2022	NUM
ap-8157	1	11	the	the	DET
ap-8157	1	12	author(s	author(s	NOUN
ap-8157	1	13	)	)	PUNCT
ap-8157	1	14	.	.	PUNCT
ap-8157	2	1	licensed	license	VERB
ap-8157	2	2	under	under	ADP
ap-8157	2	3	a	a	DET
ap-8157	2	4	cc	cc	NOUN
ap-8157	2	5	-	-	PUNCT
ap-8157	2	6	by	by	ADP
ap-8157	2	7	4.0	4.0	NUM
ap-8157	2	8	licence	licence	NOUN
ap-8157	2	9	published	publish	VERB
ap-8157	2	10	by	by	ADP
ap-8157	2	11	the	the	DET
ap-8157	2	12	czech	czech	PROPN
ap-8157	2	13	technical	technical	PROPN
ap-8157	2	14	university	university	PROPN
ap-8157	2	15	in	in	ADP
ap-8157	2	16	prague	prague	PROPN
ap-8157	2	17	determination	determination	NOUN
ap-8157	2	18	of	of	ADP
ap-8157	2	19	fan	fan	NOUN
ap-8157	2	20	design	design	NOUN
ap-8157	2	21	parameters	parameter	NOUN
ap-8157	2	22	for	for	ADP
ap-8157	2	23	light	light	ADJ
ap-8157	2	24	-	-	PUNCT
ap-8157	2	25	sport	sport	NOUN
ap-8157	2	26	aircraft	aircraft	NOUN
ap-8157	2	27	jan	jan	PROPN
ap-8157	2	28	klesa	klesa	PROPN
ap-8157	2	29	czech	czech	PROPN
ap-8157	2	30	technical	technical	PROPN
ap-8157	2	31	university	university	PROPN
ap-8157	2	32	,	,	PUNCT
ap-8157	2	33	faculty	faculty	NOUN
ap-8157	2	34	of	of	ADP
ap-8157	2	35	mechanical	mechanical	ADJ
ap-8157	2	36	engineering	engineering	NOUN
ap-8157	2	37	,	,	PUNCT
ap-8157	2	38	department	department	NOUN
ap-8157	2	39	of	of	ADP
ap-8157	2	40	aerospace	aerospace	PROPN
ap-8157	2	41	engineering	engineering	NOUN
ap-8157	2	42	,	,	PUNCT
ap-8157	2	43	karlovo	karlovo	PROPN
ap-8157	2	44	náměstí	náměstí	NOUN
ap-8157	2	45	13	13	NUM
ap-8157	2	46	,	,	PUNCT
ap-8157	2	47	prague	prague	NOUN
ap-8157	2	48	2	2	NUM
ap-8157	2	49	,	,	PUNCT
ap-8157	2	50	czech	czech	PROPN
ap-8157	2	51	republic	republic	NOUN
ap-8157	2	52	correspondence	correspondence	NOUN
ap-8157	2	53	:	:	PUNCT
ap-8157	2	54	jan.klesa@fs.cvut.cz	jan.klesa@fs.cvut.cz	PROPN
ap-8157	2	55	abstract	abstract	NOUN
ap-8157	2	56	.	.	PUNCT
ap-8157	3	1	this	this	DET
ap-8157	3	2	paper	paper	NOUN
ap-8157	3	3	is	be	AUX
ap-8157	3	4	focused	focus	VERB
ap-8157	3	5	on	on	ADP
ap-8157	3	6	the	the	DET
ap-8157	3	7	preliminary	preliminary	ADJ
ap-8157	3	8	design	design	NOUN
ap-8157	3	9	of	of	ADP
ap-8157	3	10	an	an	DET
ap-8157	3	11	electric	electric	ADJ
ap-8157	3	12	fan	fan	NOUN
ap-8157	3	13	for	for	ADP
ap-8157	3	14	light	light	ADJ
ap-8157	3	15	-	-	PUNCT
ap-8157	3	16	sport	sport	NOUN
ap-8157	3	17	aircraft	aircraft	NOUN
ap-8157	3	18	.	.	PUNCT
ap-8157	4	1	usage	usage	NOUN
ap-8157	4	2	of	of	ADP
ap-8157	4	3	electric	electric	ADJ
ap-8157	4	4	motors	motor	NOUN
ap-8157	4	5	brings	bring	VERB
ap-8157	4	6	some	some	DET
ap-8157	4	7	advantages	advantage	NOUN
ap-8157	4	8	compared	compare	VERB
ap-8157	4	9	to	to	ADP
ap-8157	4	10	piston	piston	NOUN
ap-8157	4	11	engines	engine	NOUN
ap-8157	4	12	,	,	PUNCT
ap-8157	4	13	especially	especially	ADV
ap-8157	4	14	small	small	ADJ
ap-8157	4	15	size	size	NOUN
ap-8157	4	16	and	and	CCONJ
ap-8157	4	17	the	the	DET
ap-8157	4	18	independence	independence	NOUN
ap-8157	4	19	of	of	ADP
ap-8157	4	20	power	power	NOUN
ap-8157	4	21	on	on	ADP
ap-8157	4	22	shaft	shaft	NOUN
ap-8157	4	23	rpm	rpm	NOUN
ap-8157	4	24	.	.	PUNCT
ap-8157	5	1	a	a	DET
ap-8157	5	2	1d	1d	NUM
ap-8157	5	3	compressible	compressible	ADJ
ap-8157	5	4	fluid	fluid	NOUN
ap-8157	5	5	flow	flow	NOUN
ap-8157	5	6	model	model	NOUN
ap-8157	5	7	is	be	AUX
ap-8157	5	8	used	use	VERB
ap-8157	5	9	for	for	ADP
ap-8157	5	10	the	the	DET
ap-8157	5	11	determination	determination	NOUN
ap-8157	5	12	of	of	ADP
ap-8157	5	13	the	the	DET
ap-8157	5	14	performace	performace	NOUN
ap-8157	5	15	.	.	PUNCT
ap-8157	6	1	the	the	DET
ap-8157	6	2	influence	influence	NOUN
ap-8157	6	3	of	of	ADP
ap-8157	6	4	various	various	ADJ
ap-8157	6	5	system	system	NOUN
ap-8157	6	6	parameters	parameter	NOUN
ap-8157	6	7	is	be	AUX
ap-8157	6	8	analysed	analyse	VERB
ap-8157	6	9	.	.	PUNCT
ap-8157	7	1	results	result	NOUN
ap-8157	7	2	for	for	ADP
ap-8157	7	3	the	the	DET
ap-8157	7	4	case	case	NOUN
ap-8157	7	5	of	of	ADP
ap-8157	7	6	the	the	DET
ap-8157	7	7	ul-39	ul-39	ADJ
ap-8157	7	8	ultralight	ultralight	ADJ
ap-8157	7	9	aircraft	aircraft	NOUN
ap-8157	7	10	are	be	AUX
ap-8157	7	11	presented	present	VERB
ap-8157	7	12	.	.	PUNCT
ap-8157	8	1	finally	finally	ADV
ap-8157	8	2	,	,	PUNCT
ap-8157	8	3	input	input	NOUN
ap-8157	8	4	parameters	parameter	NOUN
ap-8157	8	5	for	for	ADP
ap-8157	8	6	the	the	DET
ap-8157	8	7	fan	fan	NOUN
ap-8157	8	8	design	design	NOUN
ap-8157	8	9	are	be	AUX
ap-8157	8	10	determined	determine	VERB
ap-8157	8	11	according	accord	VERB
ap-8157	8	12	to	to	ADP
ap-8157	8	13	this	this	DET
ap-8157	8	14	analysis	analysis	NOUN
ap-8157	8	15	.	.	PUNCT
ap-8157	9	1	this	this	PRON
ap-8157	9	2	can	can	AUX
ap-8157	9	3	be	be	AUX
ap-8157	9	4	then	then	ADV
ap-8157	9	5	used	use	VERB
ap-8157	9	6	as	as	ADP
ap-8157	9	7	input	input	NOUN
ap-8157	9	8	data	datum	NOUN
ap-8157	9	9	for	for	ADP
ap-8157	9	10	the	the	DET
ap-8157	9	11	standard	standard	ADJ
ap-8157	9	12	fan	fan	NOUN
ap-8157	9	13	(	(	PUNCT
ap-8157	9	14	axial	axial	ADJ
ap-8157	9	15	compressor	compressor	NOUN
ap-8157	9	16	)	)	PUNCT
ap-8157	9	17	design	design	NOUN
ap-8157	9	18	procedure	procedure	NOUN
ap-8157	9	19	.	.	PUNCT
ap-8157	10	1	keywords	keyword	NOUN
ap-8157	10	2	:	:	PUNCT
ap-8157	10	3	ducted	ducte	VERB
ap-8157	10	4	fan	fan	PROPN
ap-8157	10	5	,	,	PUNCT
ap-8157	10	6	electric	electric	ADJ
ap-8157	10	7	propulsion	propulsion	NOUN
ap-8157	10	8	,	,	PUNCT
ap-8157	10	9	axial	axial	ADJ
ap-8157	10	10	compressor	compressor	NOUN
ap-8157	10	11	.	.	PUNCT
ap-8157	11	1	1	1	X
ap-8157	11	2	.	.	X
ap-8157	11	3	introduction	introduction	NOUN
ap-8157	11	4	electric	electric	ADJ
ap-8157	11	5	propulsion	propulsion	NOUN
ap-8157	11	6	for	for	ADP
ap-8157	11	7	aircrafts	aircraft	NOUN
ap-8157	11	8	became	become	VERB
ap-8157	11	9	a	a	DET
ap-8157	11	10	research	research	NOUN
ap-8157	11	11	topic	topic	NOUN
ap-8157	11	12	in	in	ADP
ap-8157	11	13	the	the	DET
ap-8157	11	14	last	last	ADJ
ap-8157	11	15	years	year	NOUN
ap-8157	11	16	,	,	PUNCT
ap-8157	11	17	which	which	PRON
ap-8157	11	18	is	be	AUX
ap-8157	11	19	motivated	motivate	VERB
ap-8157	11	20	by	by	ADP
ap-8157	11	21	the	the	DET
ap-8157	11	22	huge	huge	ADJ
ap-8157	11	23	progress	progress	NOUN
ap-8157	11	24	in	in	ADP
ap-8157	11	25	low	low	ADJ
ap-8157	11	26	-	-	PUNCT
ap-8157	11	27	weight	weight	NOUN
ap-8157	11	28	electric	electric	ADJ
ap-8157	11	29	power	power	NOUN
ap-8157	11	30	systems	system	NOUN
ap-8157	11	31	.	.	PUNCT
ap-8157	12	1	electric	electric	ADJ
ap-8157	12	2	flight	flight	NOUN
ap-8157	12	3	was	be	AUX
ap-8157	12	4	already	already	ADV
ap-8157	12	5	developed	develop	VERB
ap-8157	12	6	in	in	ADP
ap-8157	12	7	the	the	DET
ap-8157	12	8	1960s	1960	NOUN
ap-8157	12	9	for	for	ADP
ap-8157	12	10	radio	radio	NOUN
ap-8157	12	11	controlled	control	VERB
ap-8157	12	12	model	model	NOUN
ap-8157	12	13	aircraft	aircraft	NOUN
ap-8157	12	14	,	,	PUNCT
ap-8157	12	15	e.g.	e.g.	ADV
ap-8157	12	16	,	,	PUNCT
ap-8157	12	17	work	work	NOUN
ap-8157	12	18	of	of	ADP
ap-8157	12	19	fred	fred	PROPN
ap-8157	12	20	militky	militky	PROPN
ap-8157	13	1	[	[	X
ap-8157	13	2	1	1	NUM
ap-8157	13	3	]	]	PUNCT
ap-8157	13	4	.	.	PUNCT
ap-8157	14	1	the	the	DET
ap-8157	14	2	progress	progress	NOUN
ap-8157	14	3	in	in	ADP
ap-8157	14	4	battery	battery	NOUN
ap-8157	14	5	technology	technology	NOUN
ap-8157	14	6	(	(	PUNCT
ap-8157	14	7	from	from	ADP
ap-8157	14	8	nicd	nicd	PROPN
ap-8157	14	9	to	to	ADP
ap-8157	14	10	lithium	lithium	NOUN
ap-8157	14	11	-	-	PUNCT
ap-8157	14	12	based	base	VERB
ap-8157	14	13	batteries	battery	NOUN
ap-8157	14	14	)	)	PUNCT
ap-8157	14	15	,	,	PUNCT
ap-8157	14	16	electric	electric	PROPN
ap-8157	14	17	motors	motor	NOUN
ap-8157	14	18	(	(	PUNCT
ap-8157	14	19	from	from	ADP
ap-8157	14	20	simple	simple	ADJ
ap-8157	14	21	dc	dc	PROPN
ap-8157	14	22	brush	brush	PROPN
ap-8157	14	23	motors	motor	NOUN
ap-8157	14	24	with	with	ADP
ap-8157	14	25	ferrite	ferrite	ADJ
ap-8157	14	26	magnets	magnet	NOUN
ap-8157	14	27	,	,	PUNCT
ap-8157	14	28	later	later	ADV
ap-8157	14	29	neodymium	neodymium	NOUN
ap-8157	14	30	magnets	magnet	NOUN
ap-8157	14	31	,	,	PUNCT
ap-8157	14	32	and	and	CCONJ
ap-8157	14	33	today	today	NOUN
ap-8157	14	34	brushless	brushless	PROPN
ap-8157	14	35	dc	dc	PROPN
ap-8157	14	36	motors	motors	PROPN
ap-8157	14	37	)	)	PUNCT
ap-8157	14	38	and	and	CCONJ
ap-8157	14	39	control	control	NOUN
ap-8157	14	40	electronics	electronic	NOUN
ap-8157	14	41	led	lead	VERB
ap-8157	14	42	to	to	ADP
ap-8157	14	43	the	the	DET
ap-8157	14	44	increase	increase	NOUN
ap-8157	14	45	of	of	ADP
ap-8157	14	46	model	model	NOUN
ap-8157	14	47	performance	performance	NOUN
ap-8157	14	48	and	and	CCONJ
ap-8157	14	49	size.this	size.this	PRON
ap-8157	14	50	led	lead	VERB
ap-8157	14	51	to	to	ADP
ap-8157	14	52	the	the	DET
ap-8157	14	53	possibility	possibility	NOUN
ap-8157	14	54	of	of	ADP
ap-8157	14	55	building	build	VERB
ap-8157	14	56	manned	man	VERB
ap-8157	14	57	electrical	electrical	ADJ
ap-8157	14	58	aircrafts	aircraft	NOUN
ap-8157	14	59	in	in	ADP
ap-8157	14	60	the	the	DET
ap-8157	14	61	last	last	ADJ
ap-8157	14	62	decade	decade	NOUN
ap-8157	14	63	,	,	PUNCT
ap-8157	14	64	e.g.	e.g.	ADV
ap-8157	14	65	,	,	PUNCT
ap-8157	14	66	projects	project	NOUN
ap-8157	14	67	of	of	ADP
ap-8157	14	68	airbus	airbus	PROPN
ap-8157	14	69	,	,	PUNCT
ap-8157	14	70	pipistrel	pipistrel	NOUN
ap-8157	14	71	,	,	PUNCT
ap-8157	14	72	extra	extra	ADJ
ap-8157	14	73	,	,	PUNCT
ap-8157	14	74	jihlavan	jihlavan	NOUN
ap-8157	14	75	,	,	PUNCT
ap-8157	14	76	etc	etc	X
ap-8157	14	77	.	.	X
ap-8157	14	78	today	today	NOUN
ap-8157	14	79	,	,	PUNCT
ap-8157	14	80	the	the	DET
ap-8157	14	81	technology	technology	NOUN
ap-8157	14	82	is	be	AUX
ap-8157	14	83	advanced	advance	VERB
ap-8157	14	84	enough	enough	ADV
ap-8157	14	85	to	to	PART
ap-8157	14	86	build	build	VERB
ap-8157	14	87	a	a	DET
ap-8157	14	88	small	small	ADJ
ap-8157	14	89	fully	fully	ADV
ap-8157	14	90	-	-	PUNCT
ap-8157	14	91	electric	electric	ADJ
ap-8157	14	92	aircraft	aircraft	NOUN
ap-8157	14	93	.	.	PUNCT
ap-8157	15	1	the	the	DET
ap-8157	15	2	electric	electric	ADJ
ap-8157	15	3	propulsion	propulsion	NOUN
ap-8157	15	4	brings	bring	VERB
ap-8157	15	5	some	some	DET
ap-8157	15	6	advantages	advantage	NOUN
ap-8157	15	7	,	,	PUNCT
ap-8157	15	8	especially	especially	ADV
ap-8157	15	9	possible	possible	ADJ
ap-8157	15	10	drag	drag	NOUN
ap-8157	15	11	reduction	reduction	NOUN
ap-8157	15	12	due	due	ADP
ap-8157	15	13	to	to	ADP
ap-8157	15	14	the	the	DET
ap-8157	15	15	lower	low	ADJ
ap-8157	15	16	volume	volume	NOUN
ap-8157	15	17	and	and	CCONJ
ap-8157	15	18	cross	cross	NOUN
ap-8157	15	19	-	-	NOUN
ap-8157	15	20	section	section	NOUN
ap-8157	15	21	of	of	ADP
ap-8157	15	22	electric	electric	ADJ
ap-8157	15	23	motors	motor	NOUN
ap-8157	15	24	in	in	ADP
ap-8157	15	25	comparison	comparison	NOUN
ap-8157	15	26	with	with	ADP
ap-8157	15	27	turboprop	turboprop	NOUN
ap-8157	15	28	and	and	CCONJ
ap-8157	15	29	piston	piston	NOUN
ap-8157	15	30	engines	engine	NOUN
ap-8157	15	31	.	.	PUNCT
ap-8157	16	1	this	this	PRON
ap-8157	16	2	allows	allow	VERB
ap-8157	16	3	to	to	PART
ap-8157	16	4	decrease	decrease	VERB
ap-8157	16	5	the	the	DET
ap-8157	16	6	nacelle	nacelle	ADJ
ap-8157	16	7	size	size	NOUN
ap-8157	16	8	(	(	PUNCT
ap-8157	16	9	for	for	ADP
ap-8157	16	10	multiple	multiple	ADJ
ap-8157	16	11	engine	engine	NOUN
ap-8157	16	12	aircraft	aircraft	NOUN
ap-8157	16	13	)	)	PUNCT
ap-8157	16	14	and	and	CCONJ
ap-8157	16	15	better	well	ADJ
ap-8157	16	16	fuselage	fuselage	NOUN
ap-8157	16	17	nose	nose	NOUN
ap-8157	16	18	shape	shape	NOUN
ap-8157	16	19	(	(	PUNCT
ap-8157	16	20	for	for	ADP
ap-8157	16	21	single	single	ADJ
ap-8157	16	22	engine	engine	NOUN
ap-8157	16	23	aircraft	aircraft	NOUN
ap-8157	16	24	)	)	PUNCT
ap-8157	16	25	.	.	PUNCT
ap-8157	17	1	however	however	ADV
ap-8157	17	2	,	,	PUNCT
ap-8157	17	3	cooling	cool	VERB
ap-8157	17	4	the	the	DET
ap-8157	17	5	electric	electric	ADJ
ap-8157	17	6	components	component	NOUN
ap-8157	17	7	requires	require	VERB
ap-8157	17	8	relatively	relatively	ADV
ap-8157	17	9	large	large	ADJ
ap-8157	17	10	cooling	cool	VERB
ap-8157	17	11	systems	system	NOUN
ap-8157	17	12	because	because	SCONJ
ap-8157	17	13	of	of	ADP
ap-8157	17	14	the	the	DET
ap-8157	17	15	low	low	ADJ
ap-8157	17	16	temperature	temperature	NOUN
ap-8157	17	17	difference	difference	NOUN
ap-8157	17	18	.	.	PUNCT
ap-8157	18	1	the	the	DET
ap-8157	18	2	main	main	ADJ
ap-8157	18	3	disadvantage	disadvantage	NOUN
ap-8157	18	4	remains	remain	VERB
ap-8157	18	5	the	the	DET
ap-8157	18	6	source	source	NOUN
ap-8157	18	7	of	of	ADP
ap-8157	18	8	the	the	DET
ap-8157	18	9	electric	electric	ADJ
ap-8157	18	10	energy	energy	NOUN
ap-8157	18	11	.	.	PUNCT
ap-8157	19	1	batteries	battery	NOUN
ap-8157	19	2	are	be	AUX
ap-8157	19	3	relatively	relatively	ADV
ap-8157	19	4	heavy	heavy	ADJ
ap-8157	19	5	and	and	CCONJ
ap-8157	19	6	have	have	VERB
ap-8157	19	7	a	a	DET
ap-8157	19	8	low	low	ADJ
ap-8157	19	9	energy	energy	NOUN
ap-8157	19	10	density	density	NOUN
ap-8157	19	11	as	as	SCONJ
ap-8157	19	12	compared	compare	VERB
ap-8157	19	13	with	with	ADP
ap-8157	19	14	aircraft	aircraft	NOUN
ap-8157	19	15	fuel	fuel	NOUN
ap-8157	19	16	[	[	X
ap-8157	19	17	1	1	NUM
ap-8157	19	18	]	]	PUNCT
ap-8157	19	19	.	.	PUNCT
ap-8157	20	1	another	another	DET
ap-8157	20	2	problem	problem	NOUN
ap-8157	20	3	is	be	AUX
ap-8157	20	4	the	the	DET
ap-8157	20	5	long	long	ADJ
ap-8157	20	6	time	time	NOUN
ap-8157	20	7	necessary	necessary	ADJ
ap-8157	20	8	for	for	ADP
ap-8157	20	9	recharging	recharge	VERB
ap-8157	20	10	the	the	DET
ap-8157	20	11	batteries	battery	NOUN
ap-8157	20	12	between	between	ADP
ap-8157	20	13	flights	flight	NOUN
ap-8157	20	14	.	.	PUNCT
ap-8157	21	1	refuelling	refuelling	NOUN
ap-8157	21	2	is	be	AUX
ap-8157	21	3	usually	usually	ADV
ap-8157	21	4	much	much	ADV
ap-8157	21	5	faster	fast	ADV
ap-8157	21	6	and	and	CCONJ
ap-8157	21	7	does	do	AUX
ap-8157	21	8	not	not	PART
ap-8157	21	9	require	require	VERB
ap-8157	21	10	a	a	DET
ap-8157	21	11	high	high	ADJ
ap-8157	21	12	power	power	NOUN
ap-8157	21	13	electric	electric	ADJ
ap-8157	21	14	line	line	NOUN
ap-8157	21	15	connection	connection	NOUN
ap-8157	21	16	at	at	ADP
ap-8157	21	17	the	the	DET
ap-8157	21	18	airport	airport	NOUN
ap-8157	21	19	.	.	PUNCT
ap-8157	22	1	thus	thus	ADV
ap-8157	22	2	,	,	PUNCT
ap-8157	22	3	some	some	DET
ap-8157	22	4	hybrid	hybrid	ADJ
ap-8157	22	5	system	system	NOUN
ap-8157	22	6	using	use	VERB
ap-8157	22	7	standard	standard	ADJ
ap-8157	22	8	aircraft	aircraft	NOUN
ap-8157	22	9	fuel	fuel	NOUN
ap-8157	22	10	(	(	PUNCT
ap-8157	22	11	e.g.	e.g.	ADV
ap-8157	22	12	,	,	PUNCT
ap-8157	22	13	jet	jet	NOUN
ap-8157	22	14	-	-	PUNCT
ap-8157	22	15	a1	a1	NOUN
ap-8157	22	16	)	)	PUNCT
ap-8157	22	17	or	or	CCONJ
ap-8157	22	18	hydrogen	hydrogen	NOUN
ap-8157	22	19	is	be	AUX
ap-8157	22	20	necessary	necessary	ADJ
ap-8157	22	21	for	for	ADP
ap-8157	22	22	a	a	DET
ap-8157	22	23	long	long	ADJ
ap-8157	22	24	range	range	NOUN
ap-8157	22	25	/	/	SYM
ap-8157	22	26	high	high	ADJ
ap-8157	22	27	endurance	endurance	NOUN
ap-8157	22	28	aircraft	aircraft	NOUN
ap-8157	22	29	.	.	PUNCT
ap-8157	23	1	in	in	ADP
ap-8157	23	2	this	this	DET
ap-8157	23	3	case	case	NOUN
ap-8157	23	4	,	,	PUNCT
ap-8157	23	5	electricity	electricity	NOUN
ap-8157	23	6	is	be	AUX
ap-8157	23	7	made	make	VERB
ap-8157	23	8	onboard	onboard	ADP
ap-8157	23	9	by	by	ADP
ap-8157	23	10	means	mean	NOUN
ap-8157	23	11	of	of	ADP
ap-8157	23	12	an	an	DET
ap-8157	23	13	electric	electric	ADJ
ap-8157	23	14	generator	generator	NOUN
ap-8157	23	15	powered	power	VERB
ap-8157	23	16	by	by	ADP
ap-8157	23	17	turboshaft	turboshaft	NOUN
ap-8157	23	18	engine	engine	NOUN
ap-8157	23	19	or	or	CCONJ
ap-8157	23	20	apu	apu	PROPN
ap-8157	23	21	.	.	PUNCT
ap-8157	24	1	in	in	ADP
ap-8157	24	2	this	this	DET
ap-8157	24	3	case	case	NOUN
ap-8157	24	4	,	,	PUNCT
ap-8157	24	5	energy	energy	NOUN
ap-8157	24	6	can	can	AUX
ap-8157	24	7	be	be	AUX
ap-8157	24	8	stored	store	VERB
ap-8157	24	9	in	in	ADP
ap-8157	24	10	the	the	DET
ap-8157	24	11	high	high	ADJ
ap-8157	24	12	energy	energy	NOUN
ap-8157	24	13	density	density	NOUN
ap-8157	24	14	medium	medium	NOUN
ap-8157	24	15	,	,	PUNCT
ap-8157	24	16	but	but	CCONJ
ap-8157	24	17	the	the	DET
ap-8157	24	18	overall	overall	ADJ
ap-8157	24	19	efficiency	efficiency	NOUN
ap-8157	24	20	is	be	AUX
ap-8157	24	21	lower	low	ADJ
ap-8157	24	22	due	due	ADP
ap-8157	24	23	to	to	ADP
ap-8157	24	24	the	the	DET
ap-8157	24	25	chain	chain	NOUN
ap-8157	24	26	of	of	ADP
ap-8157	24	27	necessary	necessary	ADJ
ap-8157	24	28	energy	energy	NOUN
ap-8157	24	29	transformations	transformation	NOUN
ap-8157	24	30	.	.	PUNCT
ap-8157	25	1	both	both	DET
ap-8157	25	2	systems	system	NOUN
ap-8157	25	3	are	be	AUX
ap-8157	25	4	under	under	ADP
ap-8157	25	5	development	development	NOUN
ap-8157	25	6	for	for	ADP
ap-8157	25	7	use	use	NOUN
ap-8157	25	8	in	in	ADP
ap-8157	25	9	aviation	aviation	NOUN
ap-8157	25	10	,	,	PUNCT
ap-8157	25	11	e.g.	e.g.	ADV
ap-8157	25	12	,	,	PUNCT
ap-8157	25	13	honeywell	honeywell	PROPN
ap-8157	26	1	[	[	X
ap-8157	26	2	2	2	NUM
ap-8157	26	3	]	]	PUNCT
ap-8157	26	4	or	or	CCONJ
ap-8157	26	5	rolls	roll	NOUN
ap-8157	26	6	-	-	PUNCT
ap-8157	26	7	royce	royce	NOUN
ap-8157	26	8	[	[	X
ap-8157	26	9	3	3	NUM
ap-8157	26	10	]	]	PUNCT
ap-8157	26	11	.	.	PUNCT
ap-8157	27	1	a	a	DET
ap-8157	27	2	ducted	ducte	VERB
ap-8157	27	3	fan	fan	NOUN
ap-8157	27	4	is	be	AUX
ap-8157	27	5	used	use	VERB
ap-8157	27	6	on	on	ADP
ap-8157	27	7	electric	electric	NOUN
ap-8157	27	8	-	-	PUNCT
ap-8157	27	9	powered	power	VERB
ap-8157	27	10	"	"	PUNCT
ap-8157	27	11	jet	jet	NOUN
ap-8157	27	12	"	"	PUNCT
ap-8157	27	13	aircraft	aircraft	NOUN
ap-8157	27	14	,	,	PUNCT
ap-8157	27	15	e.g.	e.g.	ADV
ap-8157	27	16	,	,	PUNCT
ap-8157	27	17	airbus	airbus	PROPN
ap-8157	27	18	e	e	PROPN
ap-8157	27	19	-	-	PROPN
ap-8157	27	20	fan	fan	NOUN
ap-8157	27	21	.	.	PUNCT
ap-8157	28	1	a	a	DET
ap-8157	28	2	ducted	ducte	VERB
ap-8157	28	3	fan	fan	NOUN
ap-8157	28	4	allows	allow	VERB
ap-8157	28	5	the	the	DET
ap-8157	28	6	transformation	transformation	NOUN
ap-8157	28	7	of	of	ADP
ap-8157	28	8	the	the	DET
ap-8157	28	9	electric	electric	ADJ
ap-8157	28	10	energy	energy	NOUN
ap-8157	28	11	to	to	ADP
ap-8157	28	12	the	the	DET
ap-8157	28	13	propulsive	propulsive	ADJ
ap-8157	28	14	thrust	thrust	NOUN
ap-8157	28	15	at	at	ADP
ap-8157	28	16	high	high	ADJ
ap-8157	28	17	flight	flight	NOUN
ap-8157	28	18	velocity	velocity	NOUN
ap-8157	28	19	,	,	PUNCT
ap-8157	28	20	where	where	SCONJ
ap-8157	28	21	a	a	DET
ap-8157	28	22	propeller	propeller	NOUN
ap-8157	28	23	is	be	AUX
ap-8157	28	24	inefficient	inefficient	ADJ
ap-8157	28	25	.	.	PUNCT
ap-8157	29	1	it	it	PRON
ap-8157	29	2	became	become	VERB
ap-8157	29	3	a	a	DET
ap-8157	29	4	dynamic	dynamic	ADJ
ap-8157	29	5	research	research	NOUN
ap-8157	29	6	area	area	NOUN
ap-8157	29	7	in	in	ADP
ap-8157	29	8	the	the	DET
ap-8157	29	9	last	last	ADJ
ap-8157	29	10	years	year	NOUN
ap-8157	29	11	due	due	ADP
ap-8157	29	12	to	to	ADP
ap-8157	29	13	the	the	DET
ap-8157	29	14	efforts	effort	NOUN
ap-8157	29	15	of	of	ADP
ap-8157	29	16	building	build	VERB
ap-8157	29	17	electric	electric	ADJ
ap-8157	29	18	or	or	CCONJ
ap-8157	29	19	hybrid	hybrid	ADJ
ap-8157	29	20	-	-	PUNCT
ap-8157	29	21	electric	electric	ADJ
ap-8157	29	22	transport	transport	NOUN
ap-8157	29	23	aircrafts	aircraft	NOUN
ap-8157	29	24	.	.	PUNCT
ap-8157	30	1	however	however	ADV
ap-8157	30	2	,	,	PUNCT
ap-8157	30	3	ducted	ducte	VERB
ap-8157	30	4	fans	fan	NOUN
ap-8157	30	5	or	or	CCONJ
ap-8157	30	6	ducted	ducte	VERB
ap-8157	30	7	propellers	propeller	NOUN
ap-8157	30	8	have	have	VERB
ap-8157	30	9	a	a	DET
ap-8157	30	10	lower	low	ADJ
ap-8157	30	11	performance	performance	NOUN
ap-8157	30	12	at	at	ADP
ap-8157	30	13	low	low	ADJ
ap-8157	30	14	flight	flight	NOUN
ap-8157	30	15	speeds	speed	NOUN
ap-8157	30	16	for	for	ADP
ap-8157	30	17	multiple	multiple	ADJ
ap-8157	30	18	reasons	reason	NOUN
ap-8157	30	19	:	:	PUNCT
ap-8157	30	20	•	•	NUM
ap-8157	30	21	higher	high	ADJ
ap-8157	30	22	outlet	outlet	NOUN
ap-8157	30	23	velocity	velocity	NOUN
ap-8157	30	24	which	which	PRON
ap-8157	30	25	causes	cause	VERB
ap-8157	30	26	lower	low	ADJ
ap-8157	30	27	propulsive	propulsive	ADJ
ap-8157	30	28	efficiency	efficiency	NOUN
ap-8157	30	29	.	.	PUNCT
ap-8157	31	1	•	•	NUM
ap-8157	31	2	higher	high	ADJ
ap-8157	31	3	losses	loss	NOUN
ap-8157	31	4	in	in	ADP
ap-8157	31	5	the	the	DET
ap-8157	31	6	propulsion	propulsion	NOUN
ap-8157	31	7	system	system	NOUN
ap-8157	31	8	due	due	ADP
ap-8157	31	9	to	to	ADP
ap-8157	31	10	the	the	DET
ap-8157	31	11	friction	friction	NOUN
ap-8157	31	12	at	at	ADP
ap-8157	31	13	duct	duct	NOUN
ap-8157	31	14	walls	wall	NOUN
ap-8157	31	15	.	.	PUNCT
ap-8157	31	16	•	•	NUM
ap-8157	31	17	higher	high	ADJ
ap-8157	31	18	fuselage	fuselage	NOUN
ap-8157	31	19	(	(	PUNCT
ap-8157	31	20	nacelle	nacelle	NOUN
ap-8157	31	21	)	)	PUNCT
ap-8157	31	22	drag	drag	NOUN
ap-8157	31	23	.	.	PUNCT
ap-8157	32	1	•	•	NUM
ap-8157	32	2	higher	high	ADJ
ap-8157	32	3	drag	drag	NOUN
ap-8157	32	4	when	when	SCONJ
ap-8157	32	5	flying	fly	VERB
ap-8157	32	6	with	with	ADP
ap-8157	32	7	the	the	DET
ap-8157	32	8	engine	engine	NOUN
ap-8157	32	9	off	off	ADP
ap-8157	32	10	-	-	PUNCT
ap-8157	32	11	regime	regime	NOUN
ap-8157	32	12	.	.	PUNCT
ap-8157	33	1	but	but	CCONJ
ap-8157	33	2	there	there	PRON
ap-8157	33	3	is	be	VERB
ap-8157	33	4	also	also	ADV
ap-8157	33	5	some	some	DET
ap-8157	33	6	motivation	motivation	NOUN
ap-8157	33	7	for	for	ADP
ap-8157	33	8	fan	fan	NOUN
ap-8157	33	9	-	-	PUNCT
ap-8157	33	10	powered	power	VERB
ap-8157	33	11	low	low	ADJ
ap-8157	33	12	-	-	PUNCT
ap-8157	33	13	speed	speed	NOUN
ap-8157	33	14	aircraft	aircraft	NOUN
ap-8157	33	15	,	,	PUNCT
ap-8157	33	16	which	which	PRON
ap-8157	33	17	can	can	AUX
ap-8157	33	18	have	have	VERB
ap-8157	33	19	various	various	ADJ
ap-8157	33	20	advantages	advantage	NOUN
ap-8157	33	21	:	:	PUNCT
ap-8157	33	22	•	•	NUM
ap-8157	33	23	safety	safety	NOUN
ap-8157	33	24	,	,	PUNCT
ap-8157	33	25	because	because	SCONJ
ap-8157	33	26	rotating	rotate	VERB
ap-8157	33	27	parts	part	NOUN
ap-8157	33	28	are	be	AUX
ap-8157	33	29	covered	cover	VERB
ap-8157	33	30	by	by	ADP
ap-8157	33	31	the	the	DET
ap-8157	33	32	duct	duct	NOUN
ap-8157	33	33	,	,	PUNCT
ap-8157	33	34	and	and	CCONJ
ap-8157	33	35	so	so	ADV
ap-8157	33	36	the	the	DET
ap-8157	33	37	risk	risk	NOUN
ap-8157	33	38	of	of	ADP
ap-8157	33	39	damage	damage	NOUN
ap-8157	33	40	or	or	CCONJ
ap-8157	33	41	injures	injure	NOUN
ap-8157	33	42	can	can	AUX
ap-8157	33	43	be	be	AUX
ap-8157	33	44	lower	low	ADJ
ap-8157	33	45	than	than	ADP
ap-8157	33	46	for	for	ADP
ap-8157	33	47	a	a	DET
ap-8157	33	48	conventional	conventional	ADJ
ap-8157	33	49	propeller	propeller	NOUN
ap-8157	33	50	.	.	PUNCT
ap-8157	34	1	•	•	NUM
ap-8157	34	2	possible	possible	ADJ
ap-8157	34	3	noise	noise	NOUN
ap-8157	34	4	reduction	reduction	NOUN
ap-8157	34	5	.	.	PUNCT
ap-8157	35	1	•	•	NUM
ap-8157	35	2	“	"	PUNCT
ap-8157	35	3	jet	jet	NOUN
ap-8157	35	4	-	-	PUNCT
ap-8157	35	5	feeling	feeling	NOUN
ap-8157	35	6	”	"	PUNCT
ap-8157	35	7	fan	fan	NOUN
ap-8157	35	8	-	-	PUNCT
ap-8157	35	9	powered	power	VERB
ap-8157	35	10	aircraft	aircraft	NOUN
ap-8157	35	11	can	can	AUX
ap-8157	35	12	be	be	AUX
ap-8157	35	13	used	use	VERB
ap-8157	35	14	for	for	ADP
ap-8157	35	15	low	low	ADJ
ap-8157	35	16	-	-	PUNCT
ap-8157	35	17	cost	cost	NOUN
ap-8157	35	18	training	training	NOUN
ap-8157	35	19	of	of	ADP
ap-8157	35	20	jet	jet	NOUN
ap-8157	35	21	pilots	pilot	NOUN
ap-8157	35	22	.	.	PUNCT
ap-8157	36	1	the	the	DET
ap-8157	36	2	preliminary	preliminary	ADJ
ap-8157	36	3	design	design	NOUN
ap-8157	36	4	and	and	CCONJ
ap-8157	36	5	a	a	DET
ap-8157	36	6	comparison	comparison	NOUN
ap-8157	36	7	of	of	ADP
ap-8157	36	8	a	a	DET
ap-8157	36	9	ducted	ducte	VERB
ap-8157	36	10	fan	fan	NOUN
ap-8157	36	11	with	with	ADP
ap-8157	36	12	a	a	DET
ap-8157	36	13	propeller	propeller	NOUN
ap-8157	36	14	was	be	AUX
ap-8157	36	15	presented	present	VERB
ap-8157	36	16	in	in	ADP
ap-8157	36	17	[	[	X
ap-8157	36	18	4	4	NUM
ap-8157	36	19	]	]	PUNCT
ap-8157	36	20	.	.	PUNCT
ap-8157	37	1	this	this	DET
ap-8157	37	2	paper	paper	NOUN
ap-8157	37	3	is	be	AUX
ap-8157	37	4	based	base	VERB
ap-8157	37	5	on	on	ADP
ap-8157	37	6	the	the	DET
ap-8157	37	7	experience	experience	NOUN
ap-8157	37	8	with	with	ADP
ap-8157	37	9	the	the	DET
ap-8157	37	10	long	long	ADJ
ap-8157	37	11	developement	developement	NOUN
ap-8157	37	12	of	of	ADP
ap-8157	37	13	the	the	DET
ap-8157	37	14	ul-39	ul-39	ADJ
ap-8157	37	15	aircraft	aircraft	NOUN
ap-8157	37	16	at	at	ADP
ap-8157	37	17	the	the	DET
ap-8157	37	18	department	department	PROPN
ap-8157	37	19	of	of	ADP
ap-8157	37	20	aerospace	aerospace	NOUN
ap-8157	37	21	engineering	engineering	NOUN
ap-8157	37	22	of	of	ADP
ap-8157	37	23	the	the	DET
ap-8157	37	24	czech	czech	PROPN
ap-8157	37	25	technical	technical	PROPN
ap-8157	37	26	university	university	PROPN
ap-8157	37	27	in	in	ADP
ap-8157	37	28	prague	prague	PROPN
ap-8157	37	29	.	.	PUNCT
ap-8157	38	1	a	a	DET
ap-8157	38	2	more	more	ADV
ap-8157	38	3	general	general	ADJ
ap-8157	38	4	approach	approach	NOUN
ap-8157	38	5	with	with	ADP
ap-8157	38	6	a	a	DET
ap-8157	38	7	compressible	compressible	ADJ
ap-8157	38	8	fluid	fluid	NOUN
ap-8157	38	9	flow	flow	NOUN
ap-8157	38	10	model	model	NOUN
ap-8157	38	11	is	be	AUX
ap-8157	38	12	used	use	VERB
ap-8157	38	13	,	,	PUNCT
ap-8157	38	14	which	which	PRON
ap-8157	38	15	means	mean	VERB
ap-8157	38	16	549	549	NUM
ap-8157	38	17	https://doi.org/10.14311/ap.2022.62.0549	https://doi.org/10.14311/ap.2022.62.0549	PROPN
ap-8157	38	18	https://creativecommons.org/licenses/by/4.0/	https://creativecommons.org/licenses/by/4.0/	PROPN
ap-8157	38	19	https://www.cvut.cz/en	https://www.cvut.cz/en	PROPN
ap-8157	38	20	jan	jan	PROPN
ap-8157	38	21	klesa	klesa	PROPN
ap-8157	38	22	acta	acta	PROPN
ap-8157	38	23	polytechnica	polytechnica	PROPN
ap-8157	38	24	electric	electric	PROPN
ap-8157	38	25	motor−→v0	motor−→v0	X
ap-8157	38	26	−→v3	−→v3	PROPN
ap-8157	38	27	1	1	NUM
ap-8157	38	28	2	2	NUM
ap-8157	38	29	3	3	NUM
ap-8157	38	30	figure	figure	NOUN
ap-8157	38	31	1	1	NUM
ap-8157	38	32	.	.	PUNCT
ap-8157	38	33	propulsion	propulsion	NOUN
ap-8157	38	34	system	system	NOUN
ap-8157	38	35	scheme	scheme	NOUN
ap-8157	38	36	.	.	PUNCT
ap-8157	39	1	free	free	ADJ
ap-8157	39	2	atmosphere	atmosphere	NOUN
ap-8157	39	3	0	0	NUM
ap-8157	39	4	plane	plane	NOUN
ap-8157	39	5	in	in	ADP
ap-8157	39	6	front	front	NOUN
ap-8157	39	7	of	of	ADP
ap-8157	39	8	the	the	DET
ap-8157	39	9	fan	fan	NOUN
ap-8157	39	10	1	1	NUM
ap-8157	39	11	plane	plane	NOUN
ap-8157	39	12	behind	behind	ADP
ap-8157	39	13	the	the	DET
ap-8157	39	14	fan	fan	NOUN
ap-8157	39	15	2	2	NUM
ap-8157	39	16	nozzle	nozzle	NOUN
ap-8157	39	17	exit	exit	NOUN
ap-8157	39	18	3	3	NUM
ap-8157	39	19	table	table	NOUN
ap-8157	39	20	1	1	NUM
ap-8157	39	21	.	.	PUNCT
ap-8157	39	22	section	section	NOUN
ap-8157	39	23	definitions	definition	NOUN
ap-8157	39	24	.	.	PUNCT
ap-8157	40	1	that	that	SCONJ
ap-8157	40	2	this	this	DET
ap-8157	40	3	approach	approach	NOUN
ap-8157	40	4	can	can	AUX
ap-8157	40	5	also	also	ADV
ap-8157	40	6	be	be	AUX
ap-8157	40	7	used	use	VERB
ap-8157	40	8	for	for	ADP
ap-8157	40	9	a	a	DET
ap-8157	40	10	much	much	ADV
ap-8157	40	11	faster	fast	ADJ
ap-8157	40	12	aircraft	aircraft	NOUN
ap-8157	40	13	than	than	ADP
ap-8157	40	14	the	the	DET
ap-8157	40	15	ul-39	ul-39	NOUN
ap-8157	40	16	.	.	PUNCT
ap-8157	41	1	the	the	DET
ap-8157	41	2	aircraft	aircraft	NOUN
ap-8157	41	3	and	and	CCONJ
ap-8157	41	4	also	also	ADV
ap-8157	41	5	its	its	PRON
ap-8157	41	6	propulsion	propulsion	NOUN
ap-8157	41	7	system	system	NOUN
ap-8157	41	8	must	must	AUX
ap-8157	41	9	fullfill	fullfill	VERB
ap-8157	41	10	legal	legal	ADJ
ap-8157	41	11	requirements	requirement	NOUN
ap-8157	41	12	.	.	PUNCT
ap-8157	42	1	for	for	ADP
ap-8157	42	2	czech	czech	ADJ
ap-8157	42	3	ultalight	ultalight	ADJ
ap-8157	42	4	aircraft	aircraft	NOUN
ap-8157	42	5	,	,	PUNCT
ap-8157	42	6	it	it	PRON
ap-8157	42	7	is	be	AUX
ap-8157	42	8	certification	certification	NOUN
ap-8157	42	9	specification	specification	NOUN
ap-8157	42	10	ul-2	ul-2	X
ap-8157	43	1	[	[	X
ap-8157	43	2	5	5	NUM
ap-8157	43	3	]	]	PUNCT
ap-8157	43	4	(	(	PUNCT
ap-8157	43	5	requirements	requirement	NOUN
ap-8157	43	6	of	of	ADP
ap-8157	43	7	the	the	DET
ap-8157	43	8	german	german	ADJ
ap-8157	43	9	certification	certification	NOUN
ap-8157	43	10	specification	specification	NOUN
ap-8157	43	11	ltf	ltf	PROPN
ap-8157	43	12	-	-	PUNCT
ap-8157	43	13	ul	ul	PROPN
ap-8157	43	14	are	be	AUX
ap-8157	43	15	very	very	ADV
ap-8157	43	16	similar	similar	ADJ
ap-8157	43	17	[	[	X
ap-8157	43	18	6	6	NUM
ap-8157	43	19	]	]	NUM
ap-8157	43	20	)	)	PUNCT
ap-8157	43	21	.	.	PUNCT
ap-8157	44	1	this	this	PRON
ap-8157	44	2	brings	bring	VERB
ap-8157	44	3	the	the	DET
ap-8157	44	4	requirement	requirement	NOUN
ap-8157	44	5	that	that	SCONJ
ap-8157	44	6	the	the	DET
ap-8157	44	7	aircraft	aircraft	NOUN
ap-8157	44	8	has	have	VERB
ap-8157	44	9	to	to	PART
ap-8157	44	10	take	take	VERB
ap-8157	44	11	-	-	PUNCT
ap-8157	44	12	off	off	NOUN
ap-8157	44	13	on	on	ADP
ap-8157	44	14	a	a	DET
ap-8157	44	15	given	give	VERB
ap-8157	44	16	distance	distance	NOUN
ap-8157	44	17	,	,	PUNCT
ap-8157	44	18	this	this	PRON
ap-8157	44	19	creates	create	VERB
ap-8157	44	20	requirement	requirement	NOUN
ap-8157	44	21	for	for	ADP
ap-8157	44	22	thrust	thrust	NOUN
ap-8157	44	23	at	at	ADP
ap-8157	44	24	low	low	ADJ
ap-8157	44	25	speeds	speed	NOUN
ap-8157	44	26	so	so	SCONJ
ap-8157	44	27	that	that	SCONJ
ap-8157	44	28	the	the	DET
ap-8157	44	29	acceleration	acceleration	NOUN
ap-8157	44	30	is	be	AUX
ap-8157	44	31	adequate	adequate	ADJ
ap-8157	44	32	.	.	PUNCT
ap-8157	45	1	2	2	X
ap-8157	45	2	.	.	X
ap-8157	45	3	methods	method	NOUN
ap-8157	45	4	the	the	DET
ap-8157	45	5	simulation	simulation	NOUN
ap-8157	45	6	model	model	NOUN
ap-8157	45	7	is	be	AUX
ap-8157	45	8	based	base	VERB
ap-8157	45	9	on	on	ADP
ap-8157	45	10	a	a	DET
ap-8157	45	11	modified	modify	VERB
ap-8157	45	12	approach	approach	NOUN
ap-8157	45	13	from	from	ADP
ap-8157	45	14	[	[	X
ap-8157	45	15	4	4	NUM
ap-8157	45	16	]	]	PUNCT
ap-8157	45	17	based	base	VERB
ap-8157	45	18	on	on	ADP
ap-8157	45	19	experience	experience	NOUN
ap-8157	45	20	from	from	ADP
ap-8157	45	21	the	the	DET
ap-8157	45	22	developement	developement	NOUN
ap-8157	45	23	and	and	CCONJ
ap-8157	45	24	testing	testing	NOUN
ap-8157	45	25	of	of	ADP
ap-8157	45	26	the	the	DET
ap-8157	45	27	ul-39	ul-39	ADJ
ap-8157	45	28	aircraft	aircraft	NOUN
ap-8157	45	29	.	.	PUNCT
ap-8157	46	1	a	a	DET
ap-8157	46	2	compressible	compressible	ADJ
ap-8157	46	3	fluid	fluid	NOUN
ap-8157	46	4	model	model	NOUN
ap-8157	46	5	is	be	AUX
ap-8157	46	6	used	use	VERB
ap-8157	46	7	so	so	SCONJ
ap-8157	46	8	that	that	SCONJ
ap-8157	46	9	this	this	DET
ap-8157	46	10	method	method	NOUN
ap-8157	46	11	can	can	AUX
ap-8157	46	12	be	be	AUX
ap-8157	46	13	used	use	VERB
ap-8157	46	14	for	for	ADP
ap-8157	46	15	a	a	DET
ap-8157	46	16	faster	fast	ADJ
ap-8157	46	17	aircraft	aircraft	NOUN
ap-8157	46	18	than	than	ADP
ap-8157	46	19	the	the	DET
ap-8157	46	20	ultralight	ultralight	NOUN
ap-8157	46	21	cathegory	cathegory	NOUN
ap-8157	46	22	.	.	PUNCT
ap-8157	47	1	an	an	DET
ap-8157	47	2	approach	approach	NOUN
ap-8157	47	3	to	to	ADP
ap-8157	47	4	the	the	DET
ap-8157	47	5	fan	fan	NOUN
ap-8157	47	6	design	design	NOUN
ap-8157	47	7	based	base	VERB
ap-8157	47	8	on	on	ADP
ap-8157	47	9	the	the	DET
ap-8157	47	10	comparison	comparison	NOUN
ap-8157	47	11	of	of	ADP
ap-8157	47	12	various	various	ADJ
ap-8157	47	13	configurations	configuration	NOUN
ap-8157	47	14	for	for	ADP
ap-8157	47	15	the	the	DET
ap-8157	47	16	complete	complete	ADJ
ap-8157	47	17	flight	flight	NOUN
ap-8157	47	18	velocity	velocity	NOUN
ap-8157	47	19	envelope	envelope	NOUN
ap-8157	47	20	is	be	AUX
ap-8157	47	21	used	use	VERB
ap-8157	47	22	due	due	ADP
ap-8157	47	23	to	to	ADP
ap-8157	47	24	certification	certification	NOUN
ap-8157	47	25	specification	specification	NOUN
ap-8157	47	26	requirements	requirement	NOUN
ap-8157	47	27	,	,	PUNCT
ap-8157	47	28	which	which	PRON
ap-8157	47	29	are	be	AUX
ap-8157	47	30	contradictory	contradictory	ADJ
ap-8157	47	31	to	to	ADP
ap-8157	47	32	the	the	DET
ap-8157	47	33	requirement	requirement	NOUN
ap-8157	47	34	of	of	ADP
ap-8157	47	35	high	high	ADJ
ap-8157	47	36	cruise	cruise	NOUN
ap-8157	47	37	speed	speed	NOUN
ap-8157	47	38	as	as	SCONJ
ap-8157	47	39	shown	show	VERB
ap-8157	47	40	later	later	ADV
ap-8157	47	41	in	in	ADP
ap-8157	47	42	this	this	DET
ap-8157	47	43	paper	paper	NOUN
ap-8157	47	44	,	,	PUNCT
ap-8157	47	45	and	and	CCONJ
ap-8157	47	46	led	lead	VERB
ap-8157	47	47	to	to	ADP
ap-8157	47	48	the	the	DET
ap-8157	47	49	necessary	necessary	ADJ
ap-8157	47	50	modification	modification	NOUN
ap-8157	47	51	of	of	ADP
ap-8157	47	52	the	the	DET
ap-8157	47	53	approach	approach	NOUN
ap-8157	47	54	presented	present	VERB
ap-8157	47	55	in	in	ADP
ap-8157	47	56	[	[	X
ap-8157	47	57	4	4	NUM
ap-8157	47	58	]	]	PUNCT
ap-8157	47	59	.	.	PUNCT
ap-8157	48	1	an	an	DET
ap-8157	48	2	iterative	iterative	NOUN
ap-8157	48	3	method	method	NOUN
ap-8157	48	4	in	in	ADP
ap-8157	48	5	matlab	matlab	PROPN
ap-8157	48	6	is	be	AUX
ap-8157	48	7	used	use	VERB
ap-8157	48	8	for	for	ADP
ap-8157	48	9	the	the	DET
ap-8157	48	10	solution	solution	NOUN
ap-8157	48	11	of	of	ADP
ap-8157	48	12	the	the	DET
ap-8157	48	13	system	system	NOUN
ap-8157	48	14	of	of	ADP
ap-8157	48	15	equations	equation	NOUN
ap-8157	48	16	.	.	PUNCT
ap-8157	49	1	the	the	DET
ap-8157	49	2	result	result	NOUN
ap-8157	49	3	of	of	ADP
ap-8157	49	4	the	the	DET
ap-8157	49	5	method	method	NOUN
ap-8157	49	6	is	be	AUX
ap-8157	49	7	the	the	DET
ap-8157	49	8	fan	fan	PROPN
ap-8157	49	9	design	design	PROPN
ap-8157	49	10	point	point	NOUN
ap-8157	49	11	which	which	PRON
ap-8157	49	12	can	can	AUX
ap-8157	49	13	then	then	ADV
ap-8157	49	14	be	be	AUX
ap-8157	49	15	used	use	VERB
ap-8157	49	16	for	for	ADP
ap-8157	49	17	the	the	DET
ap-8157	49	18	fan	fan	PROPN
ap-8157	49	19	design	design	NOUN
ap-8157	49	20	by	by	ADP
ap-8157	49	21	standard	standard	ADJ
ap-8157	49	22	procedures	procedure	NOUN
ap-8157	49	23	,	,	PUNCT
ap-8157	49	24	see	see	VERB
ap-8157	49	25	e.g.	e.g.	ADV
ap-8157	49	26	[	[	X
ap-8157	49	27	7	7	NUM
ap-8157	49	28	]	]	PUNCT
ap-8157	49	29	and	and	CCONJ
ap-8157	49	30	[	[	X
ap-8157	49	31	8	8	NUM
ap-8157	49	32	]	]	PUNCT
ap-8157	49	33	.	.	PUNCT
ap-8157	50	1	2.1	2.1	NUM
ap-8157	50	2	.	.	PUNCT
ap-8157	50	3	physical	physical	ADJ
ap-8157	50	4	model	model	NOUN
ap-8157	50	5	the	the	DET
ap-8157	50	6	aim	aim	NOUN
ap-8157	50	7	of	of	ADP
ap-8157	50	8	the	the	DET
ap-8157	50	9	first	first	ADJ
ap-8157	50	10	step	step	NOUN
ap-8157	50	11	is	be	AUX
ap-8157	50	12	to	to	PART
ap-8157	50	13	find	find	VERB
ap-8157	50	14	parameters	parameter	NOUN
ap-8157	50	15	of	of	ADP
ap-8157	50	16	the	the	DET
ap-8157	50	17	propulsion	propulsion	NOUN
ap-8157	50	18	system	system	NOUN
ap-8157	50	19	in	in	ADP
ap-8157	50	20	design	design	NOUN
ap-8157	50	21	conditions	condition	NOUN
ap-8157	50	22	,	,	PUNCT
ap-8157	50	23	which	which	PRON
ap-8157	50	24	were	be	AUX
ap-8157	50	25	determined	determine	VERB
ap-8157	50	26	according	accord	VERB
ap-8157	50	27	to	to	ADP
ap-8157	50	28	the	the	DET
ap-8157	50	29	experience	experience	NOUN
ap-8157	50	30	with	with	ADP
ap-8157	50	31	the	the	DET
ap-8157	50	32	ul-39	ul-39	PRON
ap-8157	50	33	aircraft	aircraft	NOUN
ap-8157	50	34	testing	testing	NOUN
ap-8157	50	35	and	and	CCONJ
ap-8157	50	36	operation	operation	NOUN
ap-8157	51	1	[	[	X
ap-8157	51	2	9	9	NUM
ap-8157	51	3	]	]	PUNCT
ap-8157	51	4	.	.	PUNCT
ap-8157	52	1	it	it	PRON
ap-8157	52	2	is	be	AUX
ap-8157	52	3	a	a	DET
ap-8157	52	4	1d	1d	NUM
ap-8157	52	5	compressible	compressible	ADJ
ap-8157	52	6	fluid	fluid	ADJ
ap-8157	52	7	flow	flow	NOUN
ap-8157	52	8	model	model	NOUN
ap-8157	52	9	.	.	PUNCT
ap-8157	53	1	input	input	NOUN
ap-8157	53	2	parameters	parameter	NOUN
ap-8157	53	3	used	use	VERB
ap-8157	53	4	for	for	ADP
ap-8157	53	5	the	the	DET
ap-8157	53	6	fan	fan	NOUN
ap-8157	53	7	design	design	NOUN
ap-8157	53	8	phase	phase	NOUN
ap-8157	53	9	can	can	AUX
ap-8157	53	10	be	be	AUX
ap-8157	53	11	found	find	VERB
ap-8157	53	12	in	in	ADP
ap-8157	53	13	table	table	NOUN
ap-8157	53	14	2	2	NUM
ap-8157	53	15	.	.	PUNCT
ap-8157	54	1	the	the	DET
ap-8157	54	2	fan	fan	NOUN
ap-8157	54	3	has	have	VERB
ap-8157	54	4	to	to	PART
ap-8157	54	5	be	be	AUX
ap-8157	54	6	placed	place	VERB
ap-8157	54	7	into	into	ADP
ap-8157	54	8	the	the	DET
ap-8157	54	9	available	available	ADJ
ap-8157	54	10	space	space	NOUN
ap-8157	54	11	in	in	ADP
ap-8157	54	12	the	the	DET
ap-8157	54	13	fuselage	fuselage	NOUN
ap-8157	54	14	,	,	PUNCT
ap-8157	54	15	which	which	PRON
ap-8157	54	16	limits	limit	VERB
ap-8157	54	17	the	the	DET
ap-8157	54	18	maximal	maximal	ADJ
ap-8157	54	19	fan	fan	NOUN
ap-8157	54	20	diameter	diameter	NOUN
ap-8157	54	21	and	and	CCONJ
ap-8157	54	22	determines	determine	VERB
ap-8157	54	23	the	the	DET
ap-8157	54	24	length	length	NOUN
ap-8157	54	25	of	of	ADP
ap-8157	54	26	the	the	DET
ap-8157	54	27	exhaust	exhaust	NOUN
ap-8157	54	28	duct	duct	NOUN
ap-8157	54	29	.	.	PUNCT
ap-8157	55	1	figure	figure	NOUN
ap-8157	55	2	1	1	NUM
ap-8157	55	3	and	and	CCONJ
ap-8157	55	4	table	table	NOUN
ap-8157	55	5	1	1	NUM
ap-8157	55	6	explain	explain	VERB
ap-8157	55	7	the	the	DET
ap-8157	55	8	numbering	numbering	NOUN
ap-8157	55	9	of	of	ADP
ap-8157	55	10	different	different	ADJ
ap-8157	55	11	planes	plane	NOUN
ap-8157	55	12	in	in	ADP
ap-8157	55	13	the	the	DET
ap-8157	55	14	propulsion	propulsion	NOUN
ap-8157	55	15	system	system	NOUN
ap-8157	55	16	.	.	PUNCT
ap-8157	56	1	due	due	ADP
ap-8157	56	2	to	to	ADP
ap-8157	56	3	the	the	DET
ap-8157	56	4	complexity	complexity	NOUN
ap-8157	56	5	of	of	ADP
ap-8157	56	6	the	the	DET
ap-8157	56	7	equations	equation	NOUN
ap-8157	56	8	,	,	PUNCT
ap-8157	56	9	a	a	DET
ap-8157	56	10	numerical	numerical	ADJ
ap-8157	56	11	iterative	iterative	NOUN
ap-8157	56	12	approach	approach	NOUN
ap-8157	56	13	is	be	AUX
ap-8157	56	14	used	use	VERB
ap-8157	56	15	for	for	ADP
ap-8157	56	16	the	the	DET
ap-8157	56	17	solution	solution	NOUN
ap-8157	56	18	.	.	PUNCT
ap-8157	57	1	input	input	NOUN
ap-8157	57	2	parameters	parameter	NOUN
ap-8157	57	3	are	be	AUX
ap-8157	57	4	the	the	DET
ap-8157	57	5	fan	fan	NOUN
ap-8157	57	6	diameter	diameter	NOUN
ap-8157	57	7	d1	d1	PROPN
ap-8157	57	8	and	and	CCONJ
ap-8157	57	9	nozzle	nozzle	NOUN
ap-8157	57	10	crosssection	crosssection	NOUN
ap-8157	57	11	ratio	ratio	NOUN
ap-8157	57	12	a1	a1	PROPN
ap-8157	57	13	/	/	SYM
ap-8157	57	14	a3	a3	NOUN
ap-8157	57	15	.	.	PUNCT
ap-8157	58	1	the	the	DET
ap-8157	58	2	thrust	thrust	NOUN
ap-8157	58	3	curve	curve	NOUN
ap-8157	58	4	,	,	PUNCT
ap-8157	58	5	i.e.	i.e.	X
ap-8157	58	6	dependence	dependence	NOUN
ap-8157	58	7	of	of	ADP
ap-8157	58	8	the	the	DET
ap-8157	58	9	thrust	thrust	PROPN
ap-8157	58	10	t	t	PROPN
ap-8157	58	11	on	on	ADP
ap-8157	58	12	the	the	DET
ap-8157	58	13	flight	flight	NOUN
ap-8157	58	14	velocity	velocity	NOUN
ap-8157	58	15	v0	v0	NOUN
ap-8157	58	16	,	,	PUNCT
ap-8157	58	17	is	be	AUX
ap-8157	58	18	then	then	ADV
ap-8157	58	19	determined	determined	ADJ
ap-8157	58	20	for	for	ADP
ap-8157	58	21	every	every	DET
ap-8157	58	22	combination	combination	NOUN
ap-8157	58	23	of	of	ADP
ap-8157	58	24	d1	d1	PROPN
ap-8157	58	25	and	and	CCONJ
ap-8157	58	26	a1	a1	NOUN
ap-8157	58	27	/	/	SYM
ap-8157	58	28	a3	a3	NOUN
ap-8157	58	29	.	.	PUNCT
ap-8157	59	1	the	the	DET
ap-8157	59	2	fan	fan	PROPN
ap-8157	59	3	hub	hub	PROPN
ap-8157	59	4	-	-	PUNCT
ap-8157	59	5	to	to	ADP
ap-8157	59	6	-	-	PUNCT
ap-8157	59	7	tip	tip	NOUN
ap-8157	59	8	radius	radius	NOUN
ap-8157	59	9	ratio	ratio	NOUN
ap-8157	59	10	is	be	AUX
ap-8157	59	11	set	set	VERB
ap-8157	59	12	to	to	ADP
ap-8157	59	13	0.5	0.5	NUM
ap-8157	59	14	,	,	PUNCT
ap-8157	59	15	i.e.	i.e.	X
ap-8157	59	16	the	the	DET
ap-8157	59	17	engine	engine	NOUN
ap-8157	59	18	power	power	NOUN
ap-8157	59	19	p	p	PROPN
ap-8157	59	20	200	200	NUM
ap-8157	59	21	kw	kw	NOUN
ap-8157	59	22	flight	flight	NOUN
ap-8157	59	23	velocity	velocity	NOUN
ap-8157	59	24	range	range	NOUN
ap-8157	59	25	v0	v0	NOUN
ap-8157	59	26	0–100	0–100	PROPN
ap-8157	60	1	m	m	VERB
ap-8157	60	2	s−1	s−1	ADJ
ap-8157	60	3	air	air	NOUN
ap-8157	60	4	density	density	NOUN
ap-8157	60	5	ρ	ρ	PROPN
ap-8157	60	6	1.225	1.225	NUM
ap-8157	60	7	kg	kg	NOUN
ap-8157	60	8	m3	m3	PROPN
ap-8157	60	9	atmospheric	atmospheric	ADJ
ap-8157	60	10	pressure	pressure	NOUN
ap-8157	60	11	ps0	ps0	VERB
ap-8157	60	12	101	101	NUM
ap-8157	60	13	325	325	NUM
ap-8157	60	14	pa	pa	PROPN
ap-8157	60	15	intake	intake	PROPN
ap-8157	60	16	duct	duct	NOUN
ap-8157	60	17	pressure	pressure	NOUN
ap-8157	60	18	loss	loss	NOUN
ap-8157	60	19	coefficient	coefficient	NOUN
ap-8157	60	20	ζ01	ζ01	NOUN
ap-8157	60	21	0.1	0.1	NUM
ap-8157	60	22	fan	fan	NOUN
ap-8157	60	23	efficiency	efficiency	NOUN
ap-8157	60	24	ηfan	ηfan	NOUN
ap-8157	60	25	0.85	0.85	NUM
ap-8157	60	26	outlet	outlet	NOUN
ap-8157	60	27	duct	duct	NOUN
ap-8157	60	28	wall	wall	PROPN
ap-8157	60	29	friction	friction	PROPN
ap-8157	60	30	factor	factor	NOUN
ap-8157	60	31	λ23	λ23	PROPN
ap-8157	60	32	0.013	0.013	NUM
ap-8157	60	33	outlet	outlet	NOUN
ap-8157	60	34	duct	duct	NOUN
ap-8157	60	35	length	length	NOUN
ap-8157	60	36	l	l	PROPN
ap-8157	60	37	1.5	1.5	NUM
ap-8157	60	38	m	m	NOUN
ap-8157	60	39	air	air	NOUN
ap-8157	60	40	ratio	ratio	NOUN
ap-8157	60	41	of	of	ADP
ap-8157	60	42	specific	specific	ADJ
ap-8157	60	43	heats	heat	NOUN
ap-8157	60	44	κ	κ	PROPN
ap-8157	60	45	1.4	1.4	NUM
ap-8157	60	46	air	air	NOUN
ap-8157	60	47	specific	specific	ADJ
ap-8157	60	48	gas	gas	NOUN
ap-8157	60	49	constant	constant	ADJ
ap-8157	60	50	r	r	NOUN
ap-8157	60	51	287	287	NUM
ap-8157	60	52	j	j	NOUN
ap-8157	60	53	kg−1	kg−1	PROPN
ap-8157	60	54	k−1	k−1	PROPN
ap-8157	60	55	air	air	NOUN
ap-8157	60	56	specific	specific	ADJ
ap-8157	60	57	heat	heat	NOUN
ap-8157	60	58	at	at	ADP
ap-8157	60	59	constant	constant	ADJ
ap-8157	60	60	pressure	pressure	NOUN
ap-8157	60	61	cp	cp	NUM
ap-8157	60	62	1004.5	1004.5	NUM
ap-8157	60	63	j	j	PROPN
ap-8157	60	64	kg−1	kg−1	PROPN
ap-8157	60	65	k−1	k−1	PROPN
ap-8157	60	66	table	table	NOUN
ap-8157	60	67	2	2	NUM
ap-8157	60	68	.	.	PUNCT
ap-8157	60	69	input	input	NOUN
ap-8157	60	70	parameters	parameter	NOUN
ap-8157	60	71	for	for	ADP
ap-8157	60	72	the	the	DET
ap-8157	60	73	propulsion	propulsion	NOUN
ap-8157	60	74	system	system	NOUN
ap-8157	60	75	.	.	PUNCT
ap-8157	61	1	blade	blade	NOUN
ap-8157	61	2	length	length	NOUN
ap-8157	61	3	is	be	AUX
ap-8157	61	4	half	half	NOUN
ap-8157	61	5	of	of	ADP
ap-8157	61	6	the	the	DET
ap-8157	61	7	fan	fan	NOUN
ap-8157	61	8	radius	radius	NOUN
ap-8157	61	9	.	.	PUNCT
ap-8157	62	1	then	then	ADV
ap-8157	62	2	the	the	DET
ap-8157	62	3	fan	fan	PROPN
ap-8157	62	4	cross	cross	NOUN
ap-8157	62	5	-	-	ADJ
ap-8157	62	6	section	section	ADJ
ap-8157	62	7	a1	a1	NOUN
ap-8157	62	8	can	can	AUX
ap-8157	62	9	be	be	AUX
ap-8157	62	10	determined	determine	VERB
ap-8157	62	11	according	accord	VERB
ap-8157	62	12	to	to	ADP
ap-8157	62	13	a1	a1	NOUN
ap-8157	62	14	=	=	NOUN
ap-8157	62	15	3	3	NUM
ap-8157	62	16	4	4	NUM
ap-8157	62	17	πd2	πd2	NOUN
ap-8157	62	18	1	1	NUM
ap-8157	62	19	4	4	NUM
ap-8157	62	20	.	.	PUNCT
ap-8157	63	1	(	(	PUNCT
ap-8157	63	2	1	1	X
ap-8157	63	3	)	)	PUNCT
ap-8157	63	4	the	the	DET
ap-8157	63	5	total	total	ADJ
ap-8157	63	6	pressure	pressure	NOUN
ap-8157	63	7	in	in	ADP
ap-8157	63	8	the	the	DET
ap-8157	63	9	free	free	ADJ
ap-8157	63	10	atmosphere	atmosphere	NOUN
ap-8157	63	11	in	in	ADP
ap-8157	63	12	front	front	NOUN
ap-8157	63	13	of	of	ADP
ap-8157	63	14	the	the	DET
ap-8157	63	15	aircraft	aircraft	NOUN
ap-8157	63	16	is	be	AUX
ap-8157	63	17	detemined	detemine	VERB
ap-8157	63	18	by	by	ADP
ap-8157	63	19	the	the	DET
ap-8157	63	20	standard	standard	ADJ
ap-8157	63	21	formula	formula	NOUN
ap-8157	63	22	from	from	ADP
ap-8157	63	23	flight	flight	NOUN
ap-8157	63	24	mach	mach	NOUN
ap-8157	63	25	number	number	NOUN
ap-8157	63	26	m0	m0	NOUN
ap-8157	63	27	by	by	ADP
ap-8157	63	28	pt0	pt0	NOUN
ap-8157	63	29	=	=	SYM
ap-8157	63	30	ps0(1	ps0(1	NOUN
ap-8157	63	31	+	+	CCONJ
ap-8157	63	32	κ	κ	NOUN
ap-8157	63	33	−	−	PROPN
ap-8157	63	34	1	1	NUM
ap-8157	63	35	2	2	NUM
ap-8157	63	36	m2	m2	PROPN
ap-8157	63	37	0	0	NUM
ap-8157	63	38	)	)	PUNCT
ap-8157	63	39	κ	κ	PROPN
ap-8157	63	40	κ−1	κ−1	PROPN
ap-8157	63	41	,	,	PUNCT
ap-8157	63	42	(	(	PUNCT
ap-8157	63	43	2	2	X
ap-8157	63	44	)	)	PUNCT
ap-8157	63	45	where	where	SCONJ
ap-8157	63	46	the	the	DET
ap-8157	63	47	flight	flight	NOUN
ap-8157	63	48	mach	mach	NOUN
ap-8157	63	49	number	number	NOUN
ap-8157	63	50	m0	m0	NOUN
ap-8157	63	51	is	be	AUX
ap-8157	63	52	m0	m0	PROPN
ap-8157	63	53	=	=	SYM
ap-8157	63	54	v0	v0	PROPN
ap-8157	63	55	a0	a0	NOUN
ap-8157	63	56	(	(	PUNCT
ap-8157	63	57	3	3	NUM
ap-8157	63	58	)	)	PUNCT
ap-8157	63	59	and	and	CCONJ
ap-8157	63	60	the	the	DET
ap-8157	63	61	speed	speed	NOUN
ap-8157	63	62	of	of	ADP
ap-8157	63	63	sound	sound	NOUN
ap-8157	63	64	in	in	ADP
ap-8157	63	65	the	the	DET
ap-8157	63	66	atmosphere	atmosphere	NOUN
ap-8157	63	67	a0	a0	PROPN
ap-8157	63	68	is	be	AUX
ap-8157	63	69	a0	a0	PROPN
ap-8157	63	70	=	=	SYM
ap-8157	63	71	√	√	PROPN
ap-8157	63	72	κrts0	κrts0	PROPN
ap-8157	63	73	.	.	PUNCT
ap-8157	64	1	(	(	PUNCT
ap-8157	64	2	4	4	X
ap-8157	64	3	)	)	PUNCT
ap-8157	64	4	the	the	DET
ap-8157	64	5	total	total	ADJ
ap-8157	64	6	temperature	temperature	NOUN
ap-8157	64	7	can	can	AUX
ap-8157	64	8	be	be	AUX
ap-8157	64	9	deremined	deremine	VERB
ap-8157	64	10	in	in	ADP
ap-8157	64	11	a	a	DET
ap-8157	64	12	similar	similar	ADJ
ap-8157	64	13	way	way	NOUN
ap-8157	64	14	tt0	tt0	NOUN
ap-8157	64	15	=	=	SYM
ap-8157	65	1	ts0	ts0	PROPN
ap-8157	65	2	(	(	PUNCT
ap-8157	65	3	1	1	NUM
ap-8157	65	4	+	+	NUM
ap-8157	65	5	κ	κ	NOUN
ap-8157	65	6	−	−	NUM
ap-8157	65	7	1	1	NUM
ap-8157	65	8	2	2	NUM
ap-8157	65	9	m2	m2	PROPN
ap-8157	65	10	0	0	NUM
ap-8157	65	11	)	)	PUNCT
ap-8157	65	12	.	.	PUNCT
ap-8157	66	1	(	(	PUNCT
ap-8157	66	2	5	5	X
ap-8157	66	3	)	)	PUNCT
ap-8157	66	4	the	the	DET
ap-8157	66	5	total	total	ADJ
ap-8157	66	6	pressure	pressure	NOUN
ap-8157	66	7	in	in	ADP
ap-8157	66	8	the	the	DET
ap-8157	66	9	intake	intake	NOUN
ap-8157	66	10	duct	duct	NOUN
ap-8157	66	11	is	be	AUX
ap-8157	66	12	computed	compute	VERB
ap-8157	66	13	by	by	ADP
ap-8157	66	14	means	mean	NOUN
ap-8157	66	15	of	of	ADP
ap-8157	66	16	a	a	DET
ap-8157	66	17	loss	loss	NOUN
ap-8157	66	18	coefficient	coefficient	NOUN
ap-8157	66	19	ζ01	ζ01	NOUN
ap-8157	66	20	and	and	CCONJ
ap-8157	66	21	the	the	DET
ap-8157	66	22	fan	fan	PROPN
ap-8157	66	23	axial	axial	ADJ
ap-8157	66	24	velocity	velocity	NOUN
ap-8157	66	25	v1	v1	PROPN
ap-8157	66	26	pt1	pt1	PROPN
ap-8157	66	27	=	=	PROPN
ap-8157	66	28	pt0	pt0	PROPN
ap-8157	66	29	−	−	PROPN
ap-8157	66	30	ζ01ρ1v2	ζ01ρ1v2	PROPN
ap-8157	66	31	1	1	NUM
ap-8157	66	32	2	2	NUM
ap-8157	66	33	,	,	PUNCT
ap-8157	66	34	(	(	PUNCT
ap-8157	66	35	6	6	NUM
ap-8157	66	36	)	)	PUNCT
ap-8157	66	37	550	550	NUM
ap-8157	66	38	vol	vol	NOUN
ap-8157	66	39	.	.	PUNCT
ap-8157	67	1	62	62	NUM
ap-8157	67	2	no	no	INTJ
ap-8157	67	3	.	.	PUNCT
ap-8157	68	1	5/2022	5/2022	NOUN
ap-8157	68	2	determination	determination	NOUN
ap-8157	68	3	of	of	ADP
ap-8157	68	4	fan	fan	NOUN
ap-8157	68	5	design	design	NOUN
ap-8157	68	6	parameters	parameter	NOUN
ap-8157	68	7	for	for	ADP
ap-8157	68	8	light	light	ADJ
ap-8157	68	9	-	-	PUNCT
ap-8157	68	10	sport	sport	NOUN
ap-8157	68	11	aircraft	aircraft	NOUN
ap-8157	68	12	where	where	SCONJ
ap-8157	68	13	ζ01	ζ01	NOUN
ap-8157	68	14	=	=	NOUN
ap-8157	68	15	0.1	0.1	NUM
ap-8157	68	16	(	(	PUNCT
ap-8157	68	17	based	base	VERB
ap-8157	68	18	on	on	ADP
ap-8157	68	19	cfd	cfd	NOUN
ap-8157	68	20	simulations	simulation	NOUN
ap-8157	68	21	from	from	ADP
ap-8157	68	22	[	[	X
ap-8157	68	23	10	10	NUM
ap-8157	68	24	]	]	NUM
ap-8157	68	25	)	)	PUNCT
ap-8157	68	26	.	.	PUNCT
ap-8157	69	1	the	the	DET
ap-8157	69	2	total	total	ADJ
ap-8157	69	3	pressure	pressure	NOUN
ap-8157	69	4	recovery	recovery	NOUN
ap-8157	69	5	coefficient	coefficient	NOUN
ap-8157	69	6	(	(	PUNCT
ap-8157	69	7	see	see	VERB
ap-8157	69	8	[	[	X
ap-8157	69	9	11	11	NUM
ap-8157	69	10	]	]	PUNCT
ap-8157	69	11	)	)	PUNCT
ap-8157	69	12	can	can	AUX
ap-8157	69	13	not	not	PART
ap-8157	69	14	be	be	AUX
ap-8157	69	15	used	use	VERB
ap-8157	69	16	in	in	ADP
ap-8157	69	17	this	this	DET
ap-8157	69	18	case	case	NOUN
ap-8157	69	19	due	due	ADP
ap-8157	69	20	to	to	ADP
ap-8157	69	21	the	the	DET
ap-8157	69	22	low	low	ADJ
ap-8157	69	23	flight	flight	NOUN
ap-8157	69	24	speed	speed	NOUN
ap-8157	69	25	(	(	PUNCT
ap-8157	69	26	data	datum	NOUN
ap-8157	69	27	from	from	ADP
ap-8157	69	28	literature	literature	NOUN
ap-8157	69	29	sources	source	NOUN
ap-8157	69	30	are	be	AUX
ap-8157	69	31	suitable	suitable	ADJ
ap-8157	69	32	for	for	ADP
ap-8157	69	33	a	a	DET
ap-8157	69	34	faster	fast	ADJ
ap-8157	69	35	aircraft	aircraft	NOUN
ap-8157	69	36	)	)	PUNCT
ap-8157	69	37	.	.	PUNCT
ap-8157	70	1	heat	heat	NOUN
ap-8157	70	2	exchange	exchange	NOUN
ap-8157	70	3	in	in	ADP
ap-8157	70	4	the	the	DET
ap-8157	70	5	intake	intake	NOUN
ap-8157	70	6	duct	duct	NOUN
ap-8157	70	7	is	be	AUX
ap-8157	70	8	neglected	neglect	VERB
ap-8157	70	9	,	,	PUNCT
ap-8157	70	10	thus	thus	ADV
ap-8157	70	11	the	the	DET
ap-8157	70	12	total	total	ADJ
ap-8157	70	13	temperature	temperature	NOUN
ap-8157	70	14	remains	remain	VERB
ap-8157	70	15	the	the	DET
ap-8157	70	16	same	same	ADJ
ap-8157	70	17	tt1	tt1	NOUN
ap-8157	70	18	=	=	SYM
ap-8157	70	19	tt0	tt0	NOUN
ap-8157	70	20	.	.	PUNCT
ap-8157	71	1	(	(	PUNCT
ap-8157	71	2	7	7	X
ap-8157	71	3	)	)	PUNCT
ap-8157	71	4	the	the	DET
ap-8157	71	5	static	static	ADJ
ap-8157	71	6	temperature	temperature	NOUN
ap-8157	71	7	in	in	ADP
ap-8157	71	8	front	front	NOUN
ap-8157	71	9	of	of	ADP
ap-8157	71	10	the	the	DET
ap-8157	71	11	fan	fan	NOUN
ap-8157	71	12	is	be	AUX
ap-8157	72	1	ts1	ts1	PROPN
ap-8157	72	2	=	=	SYM
ap-8157	72	3	tt1	tt1	PROPN
ap-8157	72	4	−	−	PROPN
ap-8157	73	1	v2	v2	NOUN
ap-8157	73	2	1	1	NUM
ap-8157	73	3	2cp	2cp	NOUN
ap-8157	73	4	,	,	PUNCT
ap-8157	73	5	(	(	PUNCT
ap-8157	73	6	8)	8)	NUM
ap-8157	73	7	the	the	DET
ap-8157	73	8	speed	speed	NOUN
ap-8157	73	9	of	of	ADP
ap-8157	73	10	sound	sound	NOUN
ap-8157	73	11	is	be	AUX
ap-8157	73	12	then	then	ADV
ap-8157	73	13	a1	a1	PROPN
ap-8157	73	14	=	=	SYM
ap-8157	73	15	√	√	NUM
ap-8157	73	16	κrts1	κrts1	PROPN
ap-8157	73	17	,	,	PUNCT
ap-8157	73	18	(	(	PUNCT
ap-8157	73	19	9	9	NUM
ap-8157	73	20	)	)	PUNCT
ap-8157	73	21	and	and	CCONJ
ap-8157	73	22	the	the	DET
ap-8157	73	23	mach	mach	NOUN
ap-8157	73	24	number	number	NOUN
ap-8157	73	25	m1	m1	NOUN
ap-8157	73	26	=	=	SYM
ap-8157	73	27	v1	v1	NOUN
ap-8157	73	28	a1	a1	NOUN
ap-8157	73	29	.	.	PUNCT
ap-8157	74	1	(	(	PUNCT
ap-8157	74	2	10	10	NUM
ap-8157	74	3	)	)	PUNCT
ap-8157	74	4	the	the	DET
ap-8157	74	5	static	static	ADJ
ap-8157	74	6	pressure	pressure	NOUN
ap-8157	74	7	can	can	AUX
ap-8157	74	8	then	then	ADV
ap-8157	74	9	be	be	AUX
ap-8157	74	10	calculated	calculate	VERB
ap-8157	74	11	from	from	ADP
ap-8157	74	12	the	the	DET
ap-8157	74	13	mach	mach	NOUN
ap-8157	74	14	number	number	NOUN
ap-8157	74	15	ps1	ps1	NOUN
ap-8157	74	16	=	=	SYM
ap-8157	74	17	pt1	pt1	PROPN
ap-8157	74	18	(	(	PUNCT
ap-8157	74	19	1	1	NUM
ap-8157	74	20	+	+	NUM
ap-8157	74	21	κ	κ	NOUN
ap-8157	74	22	−	−	NUM
ap-8157	74	23	1	1	NUM
ap-8157	74	24	2	2	NUM
ap-8157	74	25	m2	m2	PROPN
ap-8157	74	26	1	1	NUM
ap-8157	74	27	)	)	PUNCT
ap-8157	74	28	−	−	PROPN
ap-8157	74	29	κ	κ	PROPN
ap-8157	74	30	κ−1	κ−1	PROPN
ap-8157	74	31	.	.	PUNCT
ap-8157	75	1	(	(	PUNCT
ap-8157	75	2	11	11	NUM
ap-8157	75	3	)	)	PUNCT
ap-8157	75	4	the	the	DET
ap-8157	75	5	density	density	NOUN
ap-8157	75	6	and	and	CCONJ
ap-8157	75	7	the	the	DET
ap-8157	75	8	air	air	NOUN
ap-8157	75	9	mass	mass	PROPN
ap-8157	75	10	flow	flow	NOUN
ap-8157	75	11	are	be	AUX
ap-8157	75	12	then	then	ADV
ap-8157	75	13	computed	compute	VERB
ap-8157	75	14	according	accord	VERB
ap-8157	75	15	to	to	ADP
ap-8157	75	16	ρ1	ρ1	NOUN
ap-8157	75	17	=	=	SYM
ap-8157	75	18	ps1	ps1	PROPN
ap-8157	75	19	rts1	rts1	NOUN
ap-8157	75	20	,	,	PUNCT
ap-8157	75	21	(	(	PUNCT
ap-8157	75	22	12	12	NUM
ap-8157	75	23	)	)	PUNCT
ap-8157	75	24	ṁ1	ṁ1	PROPN
ap-8157	75	25	=	=	SYM
ap-8157	75	26	ρ1v1a1	ρ1v1a1	PROPN
ap-8157	75	27	.	.	PUNCT
ap-8157	76	1	(	(	PUNCT
ap-8157	76	2	13	13	NUM
ap-8157	76	3	)	)	PUNCT
ap-8157	76	4	it	it	PRON
ap-8157	76	5	is	be	AUX
ap-8157	76	6	assumed	assume	VERB
ap-8157	76	7	that	that	SCONJ
ap-8157	76	8	the	the	DET
ap-8157	76	9	whole	whole	ADJ
ap-8157	76	10	engine	engine	NOUN
ap-8157	76	11	power	power	NOUN
ap-8157	76	12	p	p	NOUN
ap-8157	76	13	is	be	AUX
ap-8157	76	14	used	use	VERB
ap-8157	76	15	by	by	ADP
ap-8157	76	16	the	the	DET
ap-8157	76	17	fan	fan	NOUN
ap-8157	76	18	,	,	PUNCT
ap-8157	76	19	i.e.	i.e.	X
ap-8157	76	20	the	the	DET
ap-8157	76	21	total	total	ADJ
ap-8157	76	22	temperature	temperature	NOUN
ap-8157	76	23	is	be	AUX
ap-8157	76	24	increased	increase	VERB
ap-8157	76	25	in	in	ADP
ap-8157	76	26	the	the	DET
ap-8157	76	27	following	following	ADJ
ap-8157	76	28	way	way	NOUN
ap-8157	77	1	tt2	tt2	PROPN
ap-8157	77	2	=	=	SYM
ap-8157	77	3	tt1	tt1	PROPN
ap-8157	77	4	+	+	CCONJ
ap-8157	77	5	p	p	PROPN
ap-8157	77	6	cpρ1a1v1	cpρ1a1v1	PROPN
ap-8157	77	7	.	.	PUNCT
ap-8157	78	1	(	(	PUNCT
ap-8157	78	2	14	14	NUM
ap-8157	78	3	)	)	PUNCT
ap-8157	78	4	the	the	DET
ap-8157	78	5	total	total	ADJ
ap-8157	78	6	temperature	temperature	NOUN
ap-8157	78	7	for	for	ADP
ap-8157	78	8	isentropic	isentropic	ADJ
ap-8157	78	9	compression	compression	NOUN
ap-8157	78	10	due	due	ADP
ap-8157	78	11	to	to	ADP
ap-8157	78	12	the	the	DET
ap-8157	78	13	fan	fan	NOUN
ap-8157	78	14	is	be	AUX
ap-8157	79	1	tt2i	tt2i	PROPN
ap-8157	79	2	=	=	SYM
ap-8157	79	3	tt1	tt1	PROPN
ap-8157	79	4	+	+	CCONJ
ap-8157	79	5	ηf	ηf	PROPN
ap-8157	79	6	anp	anp	PROPN
ap-8157	79	7	cpρ1a1v1	cpρ1a1v1	PROPN
ap-8157	79	8	.	.	PUNCT
ap-8157	80	1	(	(	PUNCT
ap-8157	80	2	15	15	NUM
ap-8157	80	3	)	)	PUNCT
ap-8157	80	4	then	then	ADV
ap-8157	80	5	,	,	PUNCT
ap-8157	80	6	the	the	DET
ap-8157	80	7	total	total	ADJ
ap-8157	80	8	pressure	pressure	NOUN
ap-8157	80	9	becomes	become	VERB
ap-8157	80	10	pt2	pt2	PROPN
ap-8157	80	11	=	=	SYM
ap-8157	80	12	pt1	pt1	PROPN
ap-8157	80	13	(	(	PUNCT
ap-8157	80	14	tt2i	tt2i	PROPN
ap-8157	80	15	tt1	tt1	PROPN
ap-8157	80	16	)	)	PUNCT
ap-8157	80	17	κ	κ	PROPN
ap-8157	81	1	κ−1	κ−1	PROPN
ap-8157	81	2	,	,	PUNCT
ap-8157	81	3	(	(	PUNCT
ap-8157	81	4	16	16	NUM
ap-8157	81	5	)	)	PUNCT
ap-8157	81	6	and	and	CCONJ
ap-8157	81	7	the	the	DET
ap-8157	81	8	fan	fan	NOUN
ap-8157	81	9	pressure	pressure	NOUN
ap-8157	81	10	ratio	ratio	NOUN
ap-8157	81	11	is	be	AUX
ap-8157	81	12	π12	π12	ADJ
ap-8157	81	13	=	=	SYM
ap-8157	81	14	pt2	pt2	PROPN
ap-8157	81	15	pt1	pt1	PROPN
ap-8157	81	16	.	.	PUNCT
ap-8157	82	1	(	(	PUNCT
ap-8157	82	2	17	17	NUM
ap-8157	82	3	)	)	PUNCT
ap-8157	82	4	the	the	DET
ap-8157	82	5	stagnation	stagnation	NOUN
ap-8157	82	6	density	density	NOUN
ap-8157	82	7	behind	behind	ADP
ap-8157	82	8	the	the	DET
ap-8157	82	9	fan	fan	NOUN
ap-8157	82	10	is	be	AUX
ap-8157	82	11	ρt2	ρt2	NOUN
ap-8157	82	12	=	=	PUNCT
ap-8157	82	13	pt2	pt2	NOUN
ap-8157	82	14	rtt2	rtt2	NOUN
ap-8157	82	15	.	.	PUNCT
ap-8157	83	1	(	(	PUNCT
ap-8157	83	2	18	18	NUM
ap-8157	83	3	)	)	PUNCT
ap-8157	83	4	the	the	DET
ap-8157	83	5	critical	critical	ADJ
ap-8157	83	6	air	air	NOUN
ap-8157	83	7	density	density	NOUN
ap-8157	83	8	(	(	PUNCT
ap-8157	83	9	for	for	ADP
ap-8157	83	10	choked	choke	VERB
ap-8157	83	11	flow	flow	NOUN
ap-8157	83	12	state	state	NOUN
ap-8157	83	13	)	)	PUNCT
ap-8157	83	14	behind	behind	ADP
ap-8157	83	15	the	the	DET
ap-8157	83	16	fan	fan	NOUN
ap-8157	83	17	is	be	AUX
ap-8157	83	18	ρc2	ρc2	NOUN
ap-8157	84	1	=	=	X
ap-8157	84	2	ρt2	ρt2	NOUN
ap-8157	84	3	(	(	PUNCT
ap-8157	84	4	κ	κ	X
ap-8157	84	5	+	+	NOUN
ap-8157	84	6	1	1	NUM
ap-8157	84	7	2	2	NUM
ap-8157	84	8	)	)	PUNCT
ap-8157	84	9	−	−	PROPN
ap-8157	84	10	1	1	NUM
ap-8157	84	11	κ−1	κ−1	PROPN
ap-8157	84	12	,	,	PUNCT
ap-8157	84	13	(	(	PUNCT
ap-8157	84	14	19	19	NUM
ap-8157	84	15	)	)	PUNCT
ap-8157	84	16	and	and	CCONJ
ap-8157	84	17	the	the	DET
ap-8157	84	18	corresponding	corresponding	ADJ
ap-8157	84	19	critical	critical	ADJ
ap-8157	84	20	velocity	velocity	NOUN
ap-8157	84	21	is	be	AUX
ap-8157	84	22	vc2	vc2	NOUN
ap-8157	84	23	=	=	NOUN
ap-8157	84	24	√	√	NUM
ap-8157	84	25	2	2	NUM
ap-8157	84	26	(	(	PUNCT
ap-8157	84	27	κ	κ	NOUN
ap-8157	84	28	−	−	PROPN
ap-8157	84	29	1	1	NUM
ap-8157	84	30	)	)	PUNCT
ap-8157	84	31	cptt2	cptt2	PROPN
ap-8157	84	32	κ	κ	PROPN
ap-8157	84	33	+	+	PROPN
ap-8157	84	34	1	1	NUM
ap-8157	84	35	,	,	PUNCT
ap-8157	84	36	(	(	PUNCT
ap-8157	84	37	20	20	NUM
ap-8157	84	38	)	)	PUNCT
ap-8157	84	39	and	and	CCONJ
ap-8157	84	40	then	then	ADV
ap-8157	84	41	,	,	PUNCT
ap-8157	84	42	the	the	DET
ap-8157	84	43	critical	critical	ADJ
ap-8157	84	44	flow	flow	NOUN
ap-8157	84	45	density	density	NOUN
ap-8157	84	46	is	be	AUX
ap-8157	84	47	(	(	PUNCT
ap-8157	84	48	ρv)c2	ρv)c2	NOUN
ap-8157	84	49	=	=	PUNCT
ap-8157	84	50	vc2ρc2	vc2ρc2	NOUN
ap-8157	84	51	.	.	PUNCT
ap-8157	85	1	(	(	PUNCT
ap-8157	85	2	21	21	NUM
ap-8157	85	3	)	)	PUNCT
ap-8157	85	4	m2	m2	PROPN
ap-8157	85	5	is	be	AUX
ap-8157	85	6	computed	compute	VERB
ap-8157	85	7	so	so	SCONJ
ap-8157	85	8	that	that	SCONJ
ap-8157	85	9	the	the	DET
ap-8157	85	10	mass	mass	NOUN
ap-8157	85	11	flow	flow	NOUN
ap-8157	85	12	through	through	ADP
ap-8157	85	13	the	the	DET
ap-8157	85	14	duct	duct	NOUN
ap-8157	85	15	remains	remain	VERB
ap-8157	85	16	constant	constant	ADJ
ap-8157	85	17	.	.	PUNCT
ap-8157	86	1	i.e.	i.e.	X
ap-8157	86	2	(	(	PUNCT
ap-8157	86	3	ρv)1	ρv)1	PROPN
ap-8157	86	4	=	=	SYM
ap-8157	86	5	(	(	PUNCT
ap-8157	86	6	ρv)2	ρv)2	PROPN
ap-8157	86	7	.	.	PUNCT
ap-8157	87	1	the	the	DET
ap-8157	87	2	speed	speed	NOUN
ap-8157	87	3	of	of	ADP
ap-8157	87	4	sound	sound	NOUN
ap-8157	87	5	behind	behind	ADP
ap-8157	87	6	the	the	DET
ap-8157	87	7	fan	fan	NOUN
ap-8157	87	8	is	be	AUX
ap-8157	87	9	a2	a2	PROPN
ap-8157	87	10	=	=	PUNCT
ap-8157	87	11	vc2	vc2	PROPN
ap-8157	87	12	√	√	NUM
ap-8157	87	13	κ	κ	VERB
ap-8157	88	1	+	+	CCONJ
ap-8157	88	2	1	1	NUM
ap-8157	88	3	2	2	NUM
ap-8157	88	4	(	(	PUNCT
ap-8157	88	5	1	1	NUM
ap-8157	88	6	+	+	NUM
ap-8157	88	7	κ	κ	NOUN
ap-8157	88	8	−	−	NUM
ap-8157	88	9	1	1	NUM
ap-8157	88	10	2	2	NUM
ap-8157	88	11	m2	m2	PROPN
ap-8157	88	12	2	2	NUM
ap-8157	88	13	)	)	PUNCT
ap-8157	88	14	−1	−1	NOUN
ap-8157	88	15	.	.	PUNCT
ap-8157	89	1	(	(	PUNCT
ap-8157	89	2	22	22	NUM
ap-8157	89	3	)	)	PUNCT
ap-8157	89	4	then	then	ADV
ap-8157	89	5	,	,	PUNCT
ap-8157	89	6	the	the	DET
ap-8157	89	7	flow	flow	NOUN
ap-8157	89	8	velocity	velocity	NOUN
ap-8157	89	9	is	be	AUX
ap-8157	89	10	calculated	calculate	VERB
ap-8157	89	11	from	from	ADP
ap-8157	89	12	the	the	DET
ap-8157	89	13	mach	mach	NOUN
ap-8157	89	14	number	number	NOUN
ap-8157	89	15	m2	m2	PROPN
ap-8157	89	16	v2	v2	PROPN
ap-8157	89	17	=	=	SYM
ap-8157	89	18	m2a2	m2a2	NOUN
ap-8157	89	19	,	,	PUNCT
ap-8157	89	20	(	(	PUNCT
ap-8157	89	21	23	23	NUM
ap-8157	89	22	)	)	PUNCT
ap-8157	89	23	and	and	CCONJ
ap-8157	89	24	the	the	DET
ap-8157	89	25	air	air	NOUN
ap-8157	89	26	density	density	NOUN
ap-8157	89	27	becomes	become	VERB
ap-8157	89	28	ρ2	ρ2	NOUN
ap-8157	89	29	=	=	SYM
ap-8157	89	30	ρt2	ρt2	NOUN
ap-8157	89	31	(	(	PUNCT
ap-8157	89	32	1	1	NUM
ap-8157	90	1	+	+	NUM
ap-8157	90	2	κ	κ	NOUN
ap-8157	90	3	−	−	NUM
ap-8157	90	4	1	1	NUM
ap-8157	90	5	2	2	NUM
ap-8157	90	6	m2	m2	PROPN
ap-8157	90	7	2	2	NUM
ap-8157	90	8	)	)	PUNCT
ap-8157	90	9	−	−	PROPN
ap-8157	90	10	1	1	NUM
ap-8157	90	11	κ−1	κ−1	PROPN
ap-8157	90	12	.	.	PUNCT
ap-8157	91	1	(	(	PUNCT
ap-8157	91	2	24	24	NUM
ap-8157	91	3	)	)	PUNCT
ap-8157	91	4	the	the	DET
ap-8157	91	5	total	total	ADJ
ap-8157	91	6	pressure	pressure	NOUN
ap-8157	91	7	at	at	ADP
ap-8157	91	8	the	the	DET
ap-8157	91	9	nozzle	nozzle	NOUN
ap-8157	91	10	exit	exit	NOUN
ap-8157	91	11	3	3	NUM
ap-8157	91	12	is	be	AUX
ap-8157	91	13	computed	compute	VERB
ap-8157	91	14	from	from	ADP
ap-8157	91	15	the	the	DET
ap-8157	91	16	exhaust	exhaust	NOUN
ap-8157	91	17	duct	duct	NOUN
ap-8157	91	18	loss	loss	NOUN
ap-8157	91	19	coefficient	coefficient	NOUN
ap-8157	91	20	ζ23	ζ23	PROPN
ap-8157	91	21	pt3	pt3	NOUN
ap-8157	91	22	=	=	SYM
ap-8157	91	23	pt2	pt2	PROPN
ap-8157	92	1	−	−	PROPN
ap-8157	92	2	ζ23	ζ23	PROPN
ap-8157	92	3	ρ2v2	ρ2v2	PROPN
ap-8157	92	4	2	2	NUM
ap-8157	92	5	2	2	NUM
ap-8157	92	6	.	.	PUNCT
ap-8157	93	1	(	(	PUNCT
ap-8157	93	2	25	25	NUM
ap-8157	93	3	)	)	PUNCT
ap-8157	93	4	the	the	DET
ap-8157	93	5	value	value	NOUN
ap-8157	93	6	of	of	ADP
ap-8157	93	7	the	the	DET
ap-8157	93	8	loss	loss	NOUN
ap-8157	93	9	coefficient	coefficient	NOUN
ap-8157	93	10	ζ23	ζ23	PROPN
ap-8157	93	11	is	be	AUX
ap-8157	93	12	determined	determine	VERB
ap-8157	93	13	according	accord	VERB
ap-8157	93	14	to	to	ADP
ap-8157	93	15	the	the	DET
ap-8157	93	16	information	information	NOUN
ap-8157	93	17	from	from	ADP
ap-8157	93	18	[	[	X
ap-8157	93	19	12	12	NUM
ap-8157	93	20	]	]	PUNCT
ap-8157	93	21	.	.	PUNCT
ap-8157	94	1	the	the	DET
ap-8157	94	2	flow	flow	NOUN
ap-8157	94	3	density	density	NOUN
ap-8157	94	4	at	at	ADP
ap-8157	94	5	the	the	DET
ap-8157	94	6	nozzle	nozzle	NOUN
ap-8157	94	7	exit	exit	NOUN
ap-8157	94	8	is	be	AUX
ap-8157	94	9	computed	compute	VERB
ap-8157	94	10	from	from	ADP
ap-8157	94	11	the	the	DET
ap-8157	94	12	condition	condition	NOUN
ap-8157	94	13	of	of	ADP
ap-8157	94	14	constant	constant	ADJ
ap-8157	94	15	mass	mass	NOUN
ap-8157	94	16	flow	flow	NOUN
ap-8157	94	17	(	(	PUNCT
ap-8157	94	18	ρv)3	ρv)3	NOUN
ap-8157	94	19	=	=	SYM
ap-8157	94	20	(	(	PUNCT
ap-8157	94	21	ρv)2	ρv)2	PROPN
ap-8157	94	22	a3	a3	NOUN
ap-8157	94	23	a1	a1	NOUN
ap-8157	94	24	.	.	PUNCT
ap-8157	95	1	(	(	PUNCT
ap-8157	95	2	26	26	NUM
ap-8157	95	3	)	)	PUNCT
ap-8157	95	4	the	the	DET
ap-8157	95	5	total	total	ADJ
ap-8157	95	6	temperature	temperature	NOUN
ap-8157	95	7	behind	behind	ADP
ap-8157	95	8	the	the	DET
ap-8157	95	9	fan	fan	NOUN
ap-8157	95	10	remains	remain	VERB
ap-8157	95	11	constant	constant	ADJ
ap-8157	95	12	tt3	tt3	NOUN
ap-8157	95	13	=	=	SYM
ap-8157	95	14	tt2	tt2	PROPN
ap-8157	95	15	.	.	PROPN
ap-8157	96	1	(	(	PUNCT
ap-8157	96	2	27	27	NUM
ap-8157	96	3	)	)	PUNCT
ap-8157	96	4	the	the	DET
ap-8157	96	5	total	total	ADJ
ap-8157	96	6	air	air	NOUN
ap-8157	96	7	density	density	NOUN
ap-8157	96	8	at	at	ADP
ap-8157	96	9	the	the	DET
ap-8157	96	10	nozzle	nozzle	NOUN
ap-8157	96	11	exit	exit	NOUN
ap-8157	96	12	is	be	AUX
ap-8157	96	13	ρt3	ρt3	VERB
ap-8157	96	14	=	=	PUNCT
ap-8157	96	15	pt3	pt3	NOUN
ap-8157	96	16	rtt3	rtt3	NOUN
ap-8157	96	17	.	.	PUNCT
ap-8157	97	1	(	(	PUNCT
ap-8157	97	2	28	28	NUM
ap-8157	97	3	)	)	PUNCT
ap-8157	97	4	the	the	DET
ap-8157	97	5	critical	critical	ADJ
ap-8157	97	6	(	(	PUNCT
ap-8157	97	7	choked	choked	ADJ
ap-8157	97	8	)	)	PUNCT
ap-8157	97	9	air	air	NOUN
ap-8157	97	10	density	density	NOUN
ap-8157	97	11	in	in	ADP
ap-8157	97	12	the	the	DET
ap-8157	97	13	nozzle	nozzle	NOUN
ap-8157	97	14	exit	exit	NOUN
ap-8157	97	15	is	be	AUX
ap-8157	97	16	ρc3	ρc3	NUM
ap-8157	97	17	=	=	PRON
ap-8157	98	1	ρt3	ρt3	PRON
ap-8157	98	2	(	(	PUNCT
ap-8157	98	3	κ	κ	X
ap-8157	98	4	+	+	NOUN
ap-8157	98	5	1	1	NUM
ap-8157	98	6	2	2	NUM
ap-8157	98	7	)	)	PUNCT
ap-8157	98	8	−	−	PROPN
ap-8157	98	9	1	1	NUM
ap-8157	98	10	κ−1	κ−1	PROPN
ap-8157	98	11	,	,	PUNCT
ap-8157	98	12	(	(	PUNCT
ap-8157	98	13	29	29	NUM
ap-8157	98	14	)	)	PUNCT
ap-8157	98	15	and	and	CCONJ
ap-8157	98	16	the	the	DET
ap-8157	98	17	corresponding	corresponding	ADJ
ap-8157	98	18	critical	critical	ADJ
ap-8157	98	19	air	air	NOUN
ap-8157	98	20	velocity	velocity	NOUN
ap-8157	98	21	is	be	AUX
ap-8157	98	22	vc3	vc3	NOUN
ap-8157	98	23	=	=	PUNCT
ap-8157	99	1	√	√	NUM
ap-8157	99	2	2	2	NUM
ap-8157	99	3	(	(	PUNCT
ap-8157	99	4	κ	κ	NOUN
ap-8157	99	5	−	−	PROPN
ap-8157	99	6	1	1	NUM
ap-8157	99	7	)	)	PUNCT
ap-8157	99	8	cptt3	cptt3	NOUN
ap-8157	99	9	κ	κ	PROPN
ap-8157	100	1	+	+	ADV
ap-8157	100	2	1	1	NUM
ap-8157	100	3	,	,	PUNCT
ap-8157	100	4	(	(	PUNCT
ap-8157	100	5	30	30	NUM
ap-8157	100	6	)	)	PUNCT
ap-8157	100	7	and	and	CCONJ
ap-8157	100	8	the	the	DET
ap-8157	100	9	critical	critical	ADJ
ap-8157	100	10	flow	flow	NOUN
ap-8157	100	11	density	density	NOUN
ap-8157	100	12	is	be	AUX
ap-8157	100	13	(	(	PUNCT
ap-8157	100	14	ρv)c3	ρv)c3	PROPN
ap-8157	100	15	=	=	PUNCT
ap-8157	100	16	ρc3vc3	ρc3vc3	PROPN
ap-8157	100	17	.	.	PUNCT
ap-8157	101	1	(	(	PUNCT
ap-8157	101	2	31	31	NUM
ap-8157	101	3	)	)	SYM
ap-8157	101	4	551	551	NUM
ap-8157	101	5	jan	jan	PROPN
ap-8157	101	6	klesa	klesa	PROPN
ap-8157	101	7	acta	acta	PROPN
ap-8157	101	8	polytechnica	polytechnica	PROPN
ap-8157	101	9	figure	figure	NOUN
ap-8157	101	10	2	2	NUM
ap-8157	101	11	.	.	PUNCT
ap-8157	101	12	thrust	thrust	VERB
ap-8157	101	13	over	over	ADP
ap-8157	101	14	flight	flight	NOUN
ap-8157	101	15	speed	speed	NOUN
ap-8157	101	16	for	for	ADP
ap-8157	101	17	different	different	ADJ
ap-8157	101	18	fan	fan	NOUN
ap-8157	101	19	diameters	diameter	NOUN
ap-8157	101	20	d1	d1	NOUN
ap-8157	101	21	,	,	PUNCT
ap-8157	101	22	nozzle	nozzle	NOUN
ap-8157	101	23	contraction	contraction	NOUN
ap-8157	101	24	ratio	ratio	NOUN
ap-8157	101	25	a1	a1	PROPN
ap-8157	101	26	/	/	SYM
ap-8157	101	27	a3	a3	NOUN
ap-8157	101	28	=	=	SYM
ap-8157	101	29	1	1	X
ap-8157	101	30	.	.	X
ap-8157	101	31	figure	figure	NOUN
ap-8157	101	32	3	3	NUM
ap-8157	101	33	.	.	PUNCT
ap-8157	102	1	thrust	thrust	VERB
ap-8157	102	2	over	over	ADP
ap-8157	102	3	flight	flight	NOUN
ap-8157	102	4	speed	speed	NOUN
ap-8157	102	5	for	for	ADP
ap-8157	102	6	different	different	ADJ
ap-8157	102	7	nozzle	nozzle	NOUN
ap-8157	102	8	contraction	contraction	NOUN
ap-8157	102	9	ratios	ratios	AUX
ap-8157	102	10	a1	a1	NOUN
ap-8157	102	11	/	/	SYM
ap-8157	102	12	a3	a3	NOUN
ap-8157	102	13	,	,	PUNCT
ap-8157	102	14	fan	fan	NOUN
ap-8157	102	15	diameter	diameter	NOUN
ap-8157	102	16	d1	d1	PROPN
ap-8157	102	17	=	=	PROPN
ap-8157	102	18	0.66	0.66	NUM
ap-8157	102	19	m.	m.	NOUN
ap-8157	102	20	the	the	DET
ap-8157	102	21	static	static	ADJ
ap-8157	102	22	temperature	temperature	NOUN
ap-8157	102	23	in	in	ADP
ap-8157	102	24	the	the	DET
ap-8157	102	25	nozzle	nozzle	NOUN
ap-8157	102	26	exit	exit	NOUN
ap-8157	102	27	is	be	AUX
ap-8157	102	28	ts3	ts3	PROPN
ap-8157	102	29	=	=	SYM
ap-8157	102	30	tt3	tt3	PROPN
ap-8157	102	31	(	(	PUNCT
ap-8157	102	32	ps0	ps0	VERB
ap-8157	102	33	pt3	pt3	NOUN
ap-8157	102	34	)	)	PUNCT
ap-8157	103	1	κ−1	κ−1	PROPN
ap-8157	103	2	κ	κ	PROPN
ap-8157	103	3	,	,	PUNCT
ap-8157	103	4	(	(	PUNCT
ap-8157	103	5	32	32	NUM
ap-8157	103	6	)	)	PUNCT
ap-8157	103	7	the	the	DET
ap-8157	103	8	corresponding	corresponding	ADJ
ap-8157	103	9	speed	speed	NOUN
ap-8157	103	10	of	of	ADP
ap-8157	103	11	sound	sound	NOUN
ap-8157	103	12	is	be	AUX
ap-8157	103	13	a3	a3	NOUN
ap-8157	103	14	=	=	SYM
ap-8157	103	15	√	√	NUM
ap-8157	103	16	κrts3	κrts3	PROPN
ap-8157	103	17	,	,	PUNCT
ap-8157	103	18	(	(	PUNCT
ap-8157	103	19	33	33	NUM
ap-8157	103	20	)	)	PUNCT
ap-8157	103	21	and	and	CCONJ
ap-8157	103	22	the	the	DET
ap-8157	103	23	flow	flow	NOUN
ap-8157	103	24	velocity	velocity	NOUN
ap-8157	103	25	is	be	AUX
ap-8157	103	26	v3	v3	PROPN
ap-8157	103	27	=	=	SYM
ap-8157	104	1	m3a3	m3a3	PROPN
ap-8157	104	2	.	.	PROPN
ap-8157	104	3	(	(	PUNCT
ap-8157	104	4	34	34	NUM
ap-8157	104	5	)	)	PUNCT
ap-8157	104	6	the	the	DET
ap-8157	104	7	nozzle	nozzle	NOUN
ap-8157	104	8	exit	exit	NOUN
ap-8157	104	9	mach	mach	NOUN
ap-8157	104	10	number	number	NOUN
ap-8157	104	11	m3	m3	PROPN
ap-8157	104	12	is	be	AUX
ap-8157	104	13	determined	determine	VERB
ap-8157	104	14	from	from	ADP
ap-8157	104	15	the	the	DET
ap-8157	104	16	relation	relation	NOUN
ap-8157	104	17	between	between	ADP
ap-8157	104	18	static	static	ADJ
ap-8157	104	19	pressure	pressure	NOUN
ap-8157	104	20	ps3	ps3	NOUN
ap-8157	104	21	and	and	CCONJ
ap-8157	104	22	total	total	ADJ
ap-8157	104	23	pressure	pressure	NOUN
ap-8157	104	24	pt3	pt3	NOUN
ap-8157	104	25	ps3	ps3	NOUN
ap-8157	104	26	=	=	NOUN
ap-8157	104	27	pt3	pt3	NOUN
ap-8157	104	28	(	(	PUNCT
ap-8157	104	29	1	1	NUM
ap-8157	104	30	+	+	CCONJ
ap-8157	104	31	κ	κ	NOUN
ap-8157	104	32	−	−	NUM
ap-8157	104	33	1	1	NUM
ap-8157	104	34	2	2	NUM
ap-8157	104	35	m2	m2	PROPN
ap-8157	104	36	3	3	NUM
ap-8157	104	37	)	)	PUNCT
ap-8157	104	38	−	−	PROPN
ap-8157	104	39	κ	κ	PROPN
ap-8157	104	40	κ−1	κ−1	PROPN
ap-8157	104	41	.	.	PUNCT
ap-8157	105	1	(	(	PUNCT
ap-8157	105	2	35	35	NUM
ap-8157	105	3	)	)	PUNCT
ap-8157	105	4	the	the	DET
ap-8157	105	5	thrust	thrust	NOUN
ap-8157	105	6	of	of	ADP
ap-8157	105	7	the	the	DET
ap-8157	105	8	propulsion	propulsion	NOUN
ap-8157	105	9	system	system	NOUN
ap-8157	105	10	is	be	AUX
ap-8157	105	11	determined	determine	VERB
ap-8157	105	12	from	from	ADP
ap-8157	105	13	the	the	DET
ap-8157	105	14	momentum	momentum	NOUN
ap-8157	105	15	conservation	conservation	NOUN
ap-8157	105	16	law	law	NOUN
ap-8157	105	17	t	t	NOUN
ap-8157	105	18	=	=	SYM
ap-8157	105	19	ṁ	ṁ	PROPN
ap-8157	105	20	(	(	PUNCT
ap-8157	105	21	v3	v3	PROPN
ap-8157	105	22	−	−	PROPN
ap-8157	105	23	v0	v0	PROPN
ap-8157	105	24	)	)	PUNCT
ap-8157	105	25	,	,	PUNCT
ap-8157	105	26	(	(	PUNCT
ap-8157	105	27	36	36	NUM
ap-8157	105	28	)	)	PUNCT
ap-8157	105	29	where	where	SCONJ
ap-8157	105	30	the	the	DET
ap-8157	105	31	air	air	NOUN
ap-8157	105	32	mass	mass	PROPN
ap-8157	105	33	flow	flow	NOUN
ap-8157	105	34	is	be	AUX
ap-8157	105	35	ṁ	ṁ	NOUN
ap-8157	105	36	=	=	SYM
ap-8157	105	37	ρ1a1v1	ρ1a1v1	ADJ
ap-8157	105	38	.	.	PUNCT
ap-8157	106	1	(	(	PUNCT
ap-8157	106	2	37	37	NUM
ap-8157	106	3	)	)	PUNCT
ap-8157	106	4	finally	finally	ADV
ap-8157	106	5	,	,	PUNCT
ap-8157	106	6	the	the	DET
ap-8157	106	7	propulsion	propulsion	NOUN
ap-8157	106	8	efficiency	efficiency	NOUN
ap-8157	106	9	is	be	AUX
ap-8157	106	10	defined	define	VERB
ap-8157	106	11	by	by	ADP
ap-8157	106	12	the	the	DET
ap-8157	106	13	standard	standard	ADJ
ap-8157	106	14	formula	formula	NOUN
ap-8157	107	1	η	η	NOUN
ap-8157	107	2	=	=	PROPN
ap-8157	107	3	tv0	tv0	PROPN
ap-8157	107	4	p	p	NOUN
ap-8157	107	5	.	.	PUNCT
ap-8157	108	1	(	(	PUNCT
ap-8157	108	2	38	38	NUM
ap-8157	108	3	)	)	PUNCT
ap-8157	108	4	an	an	DET
ap-8157	108	5	iterative	iterative	NOUN
ap-8157	108	6	algorithm	algorithm	NOUN
ap-8157	108	7	has	have	VERB
ap-8157	108	8	to	to	PART
ap-8157	108	9	be	be	AUX
ap-8157	108	10	used	use	VERB
ap-8157	108	11	for	for	ADP
ap-8157	108	12	the	the	DET
ap-8157	108	13	computation	computation	NOUN
ap-8157	108	14	.	.	PUNCT
ap-8157	109	1	a	a	DET
ap-8157	109	2	value	value	NOUN
ap-8157	109	3	v1	v1	NOUN
ap-8157	109	4	=	=	SYM
ap-8157	109	5	50	50	NUM
ap-8157	109	6	m	m	NOUN
ap-8157	109	7	s−1	s−1	NOUN
ap-8157	109	8	can	can	AUX
ap-8157	109	9	be	be	AUX
ap-8157	109	10	used	use	VERB
ap-8157	109	11	as	as	ADP
ap-8157	109	12	a	a	DET
ap-8157	109	13	guess	guess	NOUN
ap-8157	109	14	for	for	ADP
ap-8157	109	15	the	the	DET
ap-8157	109	16	first	first	ADJ
ap-8157	109	17	iteration	iteration	NOUN
ap-8157	109	18	.	.	PUNCT
ap-8157	110	1	fan	fan	PROPN
ap-8157	110	2	rpm	rpm	PROPN
ap-8157	110	3	is	be	AUX
ap-8157	110	4	determined	determine	VERB
ap-8157	110	5	from	from	ADP
ap-8157	110	6	the	the	DET
ap-8157	110	7	flow	flow	NOUN
ap-8157	110	8	coefficient	coefficient	NOUN
ap-8157	110	9	ϕ	ϕ	X
ap-8157	110	10	=	=	NOUN
ap-8157	110	11	vax	vax	PROPN
ap-8157	110	12	/	/	SYM
ap-8157	110	13	u	u	PROPN
ap-8157	110	14	which	which	PRON
ap-8157	110	15	is	be	AUX
ap-8157	110	16	assumed	assume	VERB
ap-8157	110	17	to	to	PART
ap-8157	110	18	be	be	AUX
ap-8157	110	19	0.5	0.5	NUM
ap-8157	110	20	nm	nm	NOUN
ap-8157	110	21	=	=	NOUN
ap-8157	110	22	120v1	120v1	NUM
ap-8157	110	23	πd1	πd1	NOUN
ap-8157	110	24	.	.	PUNCT
ap-8157	111	1	(	(	PUNCT
ap-8157	111	2	39	39	NUM
ap-8157	111	3	)	)	PUNCT
ap-8157	111	4	3	3	NUM
ap-8157	111	5	.	.	X
ap-8157	112	1	results	result	NOUN
ap-8157	112	2	thrust	thrust	VERB
ap-8157	112	3	cuves	cuve	NOUN
ap-8157	112	4	(	(	PUNCT
ap-8157	112	5	i.e.	i.e.	X
ap-8157	112	6	dependence	dependence	NOUN
ap-8157	112	7	of	of	ADP
ap-8157	112	8	the	the	DET
ap-8157	112	9	thrust	thrust	NOUN
ap-8157	112	10	on	on	ADP
ap-8157	112	11	the	the	DET
ap-8157	112	12	flight	flight	NOUN
ap-8157	112	13	velocity	velocity	NOUN
ap-8157	112	14	)	)	PUNCT
ap-8157	112	15	for	for	ADP
ap-8157	112	16	different	different	ADJ
ap-8157	112	17	fan	fan	NOUN
ap-8157	112	18	diameters	diameter	NOUN
ap-8157	112	19	d1	d1	PROPN
ap-8157	112	20	and	and	CCONJ
ap-8157	112	21	nozzle	nozzle	NOUN
ap-8157	112	22	contraction	contraction	NOUN
ap-8157	112	23	ratios	ratio	VERB
ap-8157	112	24	a1	a1	NOUN
ap-8157	112	25	/	/	SYM
ap-8157	112	26	a3	a3	NOUN
ap-8157	112	27	are	be	AUX
ap-8157	112	28	presented	present	VERB
ap-8157	112	29	in	in	ADP
ap-8157	112	30	figures	figure	NOUN
ap-8157	112	31	2	2	NUM
ap-8157	112	32	and	and	CCONJ
ap-8157	112	33	3	3	NUM
ap-8157	112	34	.	.	PUNCT
ap-8157	112	35	an	an	DET
ap-8157	112	36	increase	increase	NOUN
ap-8157	112	37	in	in	ADP
ap-8157	112	38	fan	fan	NOUN
ap-8157	112	39	diameter	diameter	NOUN
ap-8157	112	40	d1	d1	PROPN
ap-8157	112	41	(	(	PUNCT
ap-8157	112	42	see	see	VERB
ap-8157	112	43	figure	figure	NOUN
ap-8157	112	44	2	2	NUM
ap-8157	112	45	)	)	PUNCT
ap-8157	112	46	causes	cause	VERB
ap-8157	112	47	a	a	DET
ap-8157	112	48	thrust	thrust	ADJ
ap-8157	112	49	increase	increase	NOUN
ap-8157	112	50	for	for	ADP
ap-8157	112	51	the	the	DET
ap-8157	112	52	given	give	VERB
ap-8157	112	53	velocity	velocity	NOUN
ap-8157	112	54	range	range	NOUN
ap-8157	112	55	,	,	PUNCT
ap-8157	112	56	however	however	ADV
ap-8157	112	57	,	,	PUNCT
ap-8157	112	58	this	this	DET
ap-8157	112	59	influence	influence	NOUN
ap-8157	112	60	diminishes	diminish	VERB
ap-8157	112	61	with	with	ADP
ap-8157	112	62	increasing	increase	VERB
ap-8157	112	63	flight	flight	NOUN
ap-8157	112	64	velocity	velocity	NOUN
ap-8157	112	65	as	as	SCONJ
ap-8157	112	66	expected	expect	VERB
ap-8157	112	67	from	from	ADP
ap-8157	112	68	the	the	DET
ap-8157	112	69	general	general	ADJ
ap-8157	112	70	theory	theory	NOUN
ap-8157	112	71	of	of	ADP
ap-8157	112	72	aerospace	aerospace	NOUN
ap-8157	112	73	propulsion	propulsion	NOUN
ap-8157	112	74	.	.	PUNCT
ap-8157	113	1	the	the	DET
ap-8157	113	2	influence	influence	NOUN
ap-8157	113	3	of	of	ADP
ap-8157	113	4	nozzle	nozzle	NOUN
ap-8157	113	5	contraction	contraction	NOUN
ap-8157	113	6	ratios	ratio	VERB
ap-8157	113	7	a1	a1	NOUN
ap-8157	113	8	/	/	SYM
ap-8157	113	9	a3	a3	NOUN
ap-8157	113	10	on	on	ADP
ap-8157	113	11	thrust	thrust	PROPN
ap-8157	113	12	(	(	PUNCT
ap-8157	113	13	see	see	VERB
ap-8157	113	14	figure	figure	NOUN
ap-8157	113	15	3	3	NUM
ap-8157	113	16	)	)	PUNCT
ap-8157	113	17	is	be	AUX
ap-8157	113	18	similar	similar	ADJ
ap-8157	113	19	.	.	PUNCT
ap-8157	114	1	lower	low	ADJ
ap-8157	114	2	a1	a1	NOUN
ap-8157	114	3	/	/	SYM
ap-8157	114	4	a3	a3	NOUN
ap-8157	114	5	leads	lead	VERB
ap-8157	114	6	to	to	ADP
ap-8157	114	7	a	a	DET
ap-8157	114	8	higher	high	ADJ
ap-8157	114	9	thrust	thrust	NOUN
ap-8157	114	10	at	at	ADP
ap-8157	114	11	a	a	DET
ap-8157	114	12	lower	low	ADJ
ap-8157	114	13	flight	flight	NOUN
ap-8157	114	14	velocity	velocity	NOUN
ap-8157	114	15	,	,	PUNCT
ap-8157	114	16	but	but	CCONJ
ap-8157	114	17	reduces	reduce	VERB
ap-8157	114	18	the	the	DET
ap-8157	114	19	flight	flight	NOUN
ap-8157	114	20	performance	performance	NOUN
ap-8157	114	21	at	at	ADP
ap-8157	114	22	a	a	DET
ap-8157	114	23	higher	high	ADJ
ap-8157	114	24	velocity	velocity	NOUN
ap-8157	114	25	.	.	PUNCT
ap-8157	115	1	the	the	DET
ap-8157	115	2	influence	influence	NOUN
ap-8157	115	3	of	of	ADP
ap-8157	115	4	the	the	DET
ap-8157	115	5	fan	fan	NOUN
ap-8157	115	6	diameter	diameter	NOUN
ap-8157	115	7	d1	d1	PROPN
ap-8157	115	8	and	and	CCONJ
ap-8157	115	9	nozzle	nozzle	NOUN
ap-8157	115	10	contraction	contraction	NOUN
ap-8157	115	11	ratio	ratio	NOUN
ap-8157	115	12	a1	a1	PROPN
ap-8157	115	13	/	/	SYM
ap-8157	115	14	a3	a3	NOUN
ap-8157	115	15	on	on	ADP
ap-8157	115	16	the	the	DET
ap-8157	115	17	efficiency	efficiency	NOUN
ap-8157	115	18	is	be	AUX
ap-8157	115	19	presented	present	VERB
ap-8157	115	20	in	in	ADP
ap-8157	115	21	figures	figure	NOUN
ap-8157	115	22	4	4	NUM
ap-8157	115	23	and	and	CCONJ
ap-8157	115	24	5	5	NUM
ap-8157	115	25	.	.	PUNCT
ap-8157	116	1	the	the	DET
ap-8157	116	2	efficiency	efficiency	NOUN
ap-8157	116	3	is	be	AUX
ap-8157	116	4	relatively	relatively	ADV
ap-8157	116	5	low	low	ADJ
ap-8157	116	6	in	in	ADP
ap-8157	116	7	comparison	comparison	NOUN
ap-8157	116	8	with	with	ADP
ap-8157	116	9	the	the	DET
ap-8157	116	10	standard	standard	ADJ
ap-8157	116	11	propeller	propeller	NOUN
ap-8157	116	12	due	due	ADP
ap-8157	116	13	to	to	ADP
ap-8157	116	14	the	the	DET
ap-8157	116	15	small	small	PROPN
ap-8157	116	16	fan	fan	PROPN
ap-8157	116	17	cross	cross	ADJ
ap-8157	116	18	-	-	ADJ
ap-8157	116	19	section	section	ADJ
ap-8157	116	20	area	area	NOUN
ap-8157	116	21	and	and	CCONJ
ap-8157	116	22	also	also	ADV
ap-8157	116	23	due	due	ADP
ap-8157	116	24	to	to	ADP
ap-8157	116	25	the	the	DET
ap-8157	116	26	viscous	viscous	ADJ
ap-8157	116	27	losses	loss	NOUN
ap-8157	116	28	in	in	ADP
ap-8157	116	29	the	the	DET
ap-8157	116	30	duct	duct	NOUN
ap-8157	116	31	system	system	NOUN
ap-8157	116	32	.	.	PUNCT
ap-8157	117	1	another	another	DET
ap-8157	117	2	important	important	ADJ
ap-8157	117	3	parameter	parameter	NOUN
ap-8157	117	4	for	for	ADP
ap-8157	117	5	the	the	DET
ap-8157	117	6	fan	fan	NOUN
ap-8157	117	7	design	design	NOUN
ap-8157	117	8	is	be	AUX
ap-8157	117	9	the	the	DET
ap-8157	117	10	axial	axial	ADJ
ap-8157	117	11	velocity	velocity	NOUN
ap-8157	117	12	v1	v1	NOUN
ap-8157	117	13	presented	present	VERB
ap-8157	117	14	in	in	ADP
ap-8157	117	15	figures	figure	NOUN
ap-8157	117	16	6	6	NUM
ap-8157	117	17	and	and	CCONJ
ap-8157	117	18	7	7	NUM
ap-8157	117	19	.	.	X
ap-8157	118	1	it	it	PRON
ap-8157	118	2	is	be	AUX
ap-8157	118	3	clearly	clearly	ADV
ap-8157	118	4	visible	visible	ADJ
ap-8157	118	5	that	that	SCONJ
ap-8157	118	6	there	there	PRON
ap-8157	118	7	is	be	VERB
ap-8157	118	8	a	a	DET
ap-8157	118	9	strong	strong	ADJ
ap-8157	118	10	dependence	dependence	NOUN
ap-8157	118	11	of	of	ADP
ap-8157	118	12	the	the	DET
ap-8157	118	13	fan	fan	PROPN
ap-8157	118	14	axial	axial	ADJ
ap-8157	118	15	velocity	velocity	NOUN
ap-8157	118	16	v1	v1	NOUN
ap-8157	118	17	on	on	ADP
ap-8157	118	18	constant	constant	ADJ
ap-8157	118	19	electric	electric	ADJ
ap-8157	118	20	motor	motor	NOUN
ap-8157	118	21	power	power	NOUN
ap-8157	118	22	.	.	PUNCT
ap-8157	119	1	both	both	DET
ap-8157	119	2	parameters	parameter	NOUN
ap-8157	119	3	,	,	PUNCT
ap-8157	119	4	i.e.	i.e.	X
ap-8157	119	5	fan	fan	NOUN
ap-8157	119	6	diameter	diameter	NOUN
ap-8157	119	7	d1	d1	PROPN
ap-8157	119	8	and	and	CCONJ
ap-8157	119	9	nozzle	nozzle	NOUN
ap-8157	119	10	contraction	contraction	NOUN
ap-8157	119	11	ratio	ratio	NOUN
ap-8157	119	12	a1	a1	PROPN
ap-8157	119	13	/	/	SYM
ap-8157	119	14	a3	a3	NOUN
ap-8157	119	15	,	,	PUNCT
ap-8157	119	16	have	have	VERB
ap-8157	119	17	a	a	DET
ap-8157	119	18	strong	strong	ADJ
ap-8157	119	19	influence	influence	NOUN
ap-8157	119	20	on	on	ADP
ap-8157	119	21	v1	v1	NOUN
ap-8157	119	22	.	.	PUNCT
ap-8157	120	1	the	the	DET
ap-8157	120	2	dependence	dependence	NOUN
ap-8157	120	3	of	of	ADP
ap-8157	120	4	the	the	DET
ap-8157	120	5	fan	fan	NOUN
ap-8157	120	6	pressure	pressure	NOUN
ap-8157	120	7	ratio	ratio	NOUN
ap-8157	120	8	on	on	ADP
ap-8157	120	9	the	the	DET
ap-8157	120	10	flight	flight	NOUN
ap-8157	120	11	velocity	velocity	NOUN
ap-8157	120	12	and	and	CCONJ
ap-8157	120	13	fan	fan	NOUN
ap-8157	120	14	diameter	diameter	NOUN
ap-8157	120	15	is	be	AUX
ap-8157	120	16	presented	present	VERB
ap-8157	120	17	in	in	ADP
ap-8157	120	18	figure	figure	NOUN
ap-8157	120	19	8	8	NUM
ap-8157	120	20	.	.	PUNCT
ap-8157	121	1	the	the	DET
ap-8157	121	2	fan	fan	NOUN
ap-8157	121	3	rpm	rpm	NOUN
ap-8157	121	4	for	for	ADP
ap-8157	121	5	the	the	DET
ap-8157	121	6	same	same	ADJ
ap-8157	121	7	situation	situation	NOUN
ap-8157	121	8	is	be	AUX
ap-8157	121	9	presented	present	VERB
ap-8157	121	10	in	in	ADP
ap-8157	121	11	figure	figure	NOUN
ap-8157	121	12	9	9	NUM
ap-8157	121	13	(	(	PUNCT
ap-8157	121	14	the	the	DET
ap-8157	121	15	assumption	assumption	NOUN
ap-8157	121	16	of	of	ADP
ap-8157	121	17	constant	constant	ADJ
ap-8157	121	18	ϕ	ϕ	X
ap-8157	121	19	=	=	PUNCT
ap-8157	121	20	vax	vax	PROPN
ap-8157	121	21	/	/	SYM
ap-8157	121	22	u	u	NOUN
ap-8157	121	23	=	=	NOUN
ap-8157	121	24	0.5	0.5	NUM
ap-8157	121	25	is	be	AUX
ap-8157	121	26	used	use	VERB
ap-8157	121	27	)	)	PUNCT
ap-8157	121	28	.	.	PUNCT
ap-8157	122	1	based	base	VERB
ap-8157	122	2	on	on	ADP
ap-8157	122	3	the	the	DET
ap-8157	122	4	above	above	ADV
ap-8157	122	5	-	-	PUNCT
ap-8157	122	6	mentioned	mention	VERB
ap-8157	122	7	results	result	NOUN
ap-8157	122	8	,	,	PUNCT
ap-8157	122	9	the	the	DET
ap-8157	122	10	dependencies	dependency	NOUN
ap-8157	122	11	of	of	ADP
ap-8157	122	12	fan	fan	NOUN
ap-8157	122	13	pressure	pressure	NOUN
ap-8157	122	14	ratio	ratio	NOUN
ap-8157	122	15	π	π	PROPN
ap-8157	122	16	,	,	PUNCT
ap-8157	122	17	thrust	thrust	VERB
ap-8157	122	18	t	t	PROPN
ap-8157	122	19	,	,	PUNCT
ap-8157	122	20	fan	fan	PROPN
ap-8157	122	21	axial	axial	ADJ
ap-8157	122	22	velocity	velocity	NOUN
ap-8157	122	23	v1	v1	NOUN
ap-8157	122	24	and	and	CCONJ
ap-8157	122	25	fan	fan	NOUN
ap-8157	122	26	rpm	rpm	PROPN
ap-8157	122	27	nm	nm	PROPN
ap-8157	122	28	on	on	ADP
ap-8157	122	29	the	the	DET
ap-8157	122	30	fan	fan	NOUN
ap-8157	122	31	diameter	diameter	NOUN
ap-8157	122	32	d	d	NOUN
ap-8157	122	33	and	and	CCONJ
ap-8157	122	34	nozzle	nozzle	NOUN
ap-8157	122	35	contraction	contraction	NOUN
ap-8157	122	36	ratio	ratio	NOUN
ap-8157	122	37	a1	a1	PROPN
ap-8157	122	38	/	/	SYM
ap-8157	122	39	a3	a3	NOUN
ap-8157	122	40	for	for	ADP
ap-8157	122	41	static	static	ADJ
ap-8157	122	42	case	case	NOUN
ap-8157	122	43	(	(	PUNCT
ap-8157	122	44	i.e.	i.e.	X
ap-8157	122	45	v0	v0	NOUN
ap-8157	122	46	=	=	SYM
ap-8157	122	47	0	0	NUM
ap-8157	122	48	km	km	PROPN
ap-8157	122	49	h−1	h−1	PROPN
ap-8157	122	50	,	,	PUNCT
ap-8157	122	51	take	take	VERB
ap-8157	122	52	-	-	PUNCT
ap-8157	122	53	off	off	NOUN
ap-8157	122	54	)	)	PUNCT
ap-8157	122	55	and	and	CCONJ
ap-8157	122	56	for	for	ADP
ap-8157	122	57	maximum	maximum	ADJ
ap-8157	122	58	flight	flight	NOUN
ap-8157	122	59	velocity	velocity	NOUN
ap-8157	122	60	(	(	PUNCT
ap-8157	122	61	i.e.	i.e.	X
ap-8157	122	62	v0	v0	NOUN
ap-8157	122	63	=	=	SYM
ap-8157	122	64	300	300	NUM
ap-8157	122	65	km	km	NOUN
ap-8157	122	66	h−1	h−1	PROPN
ap-8157	122	67	)	)	PUNCT
ap-8157	122	68	,	,	PUNCT
ap-8157	122	69	are	be	AUX
ap-8157	122	70	presented	present	VERB
ap-8157	122	71	in	in	ADP
ap-8157	122	72	figures	figure	NOUN
ap-8157	122	73	10–17	10–17	NUM
ap-8157	122	74	.	.	PUNCT
ap-8157	123	1	based	base	VERB
ap-8157	123	2	on	on	ADP
ap-8157	123	3	this	this	PRON
ap-8157	123	4	and	and	CCONJ
ap-8157	123	5	the	the	DET
ap-8157	123	6	fuselage	fuselage	NOUN
ap-8157	123	7	geometry	geometry	NOUN
ap-8157	123	8	,	,	PUNCT
ap-8157	123	9	a	a	DET
ap-8157	123	10	fan	fan	NOUN
ap-8157	123	11	diameter	diameter	NOUN
ap-8157	123	12	of	of	ADP
ap-8157	123	13	d1	d1	PROPN
ap-8157	123	14	=	=	PROPN
ap-8157	123	15	0.66	0.66	NUM
ap-8157	123	16	m	m	VERB
ap-8157	123	17	was	be	AUX
ap-8157	123	18	selected	select	VERB
ap-8157	123	19	.	.	PUNCT
ap-8157	124	1	the	the	DET
ap-8157	124	2	ratio	ratio	NOUN
ap-8157	124	3	a1	a1	PROPN
ap-8157	124	4	/	/	SYM
ap-8157	124	5	a3	a3	NOUN
ap-8157	124	6	is	be	AUX
ap-8157	124	7	determined	determine	VERB
ap-8157	124	8	from	from	ADP
ap-8157	124	9	the	the	DET
ap-8157	124	10	relative	relative	ADJ
ap-8157	124	11	thrust	thrust	NOUN
ap-8157	124	12	shown	show	VERB
ap-8157	124	13	in	in	ADP
ap-8157	124	14	figure	figure	NOUN
ap-8157	124	15	18	18	NUM
ap-8157	124	16	.	.	PUNCT
ap-8157	125	1	the	the	DET
ap-8157	125	2	relative	relative	ADJ
ap-8157	125	3	thrust	thrust	NOUN
ap-8157	125	4	is	be	AUX
ap-8157	125	5	defined	define	VERB
ap-8157	125	6	as	as	ADP
ap-8157	125	7	the	the	DET
ap-8157	125	8	ratio	ratio	NOUN
ap-8157	125	9	t	t	PROPN
ap-8157	125	10	/	/	SYM
ap-8157	125	11	tref	tref	NOUN
ap-8157	125	12	,	,	PUNCT
ap-8157	125	13	where	where	SCONJ
ap-8157	125	14	the	the	DET
ap-8157	125	15	reference	reference	NOUN
ap-8157	125	16	value	value	NOUN
ap-8157	125	17	tref	tref	NOUN
ap-8157	125	18	is	be	AUX
ap-8157	125	19	552	552	NUM
ap-8157	125	20	vol	vol	NOUN
ap-8157	125	21	.	.	PUNCT
ap-8157	126	1	62	62	NUM
ap-8157	126	2	no	no	INTJ
ap-8157	126	3	.	.	PUNCT
ap-8157	127	1	5/2022	5/2022	NOUN
ap-8157	127	2	determination	determination	NOUN
ap-8157	127	3	of	of	ADP
ap-8157	127	4	fan	fan	NOUN
ap-8157	127	5	design	design	NOUN
ap-8157	127	6	parameters	parameter	NOUN
ap-8157	127	7	for	for	ADP
ap-8157	127	8	light	light	ADJ
ap-8157	127	9	-	-	PUNCT
ap-8157	127	10	sport	sport	NOUN
ap-8157	127	11	aircraft	aircraft	NOUN
ap-8157	127	12	figure	figure	NOUN
ap-8157	127	13	4	4	NUM
ap-8157	127	14	.	.	PUNCT
ap-8157	127	15	efficiency	efficiency	NOUN
ap-8157	127	16	of	of	ADP
ap-8157	127	17	the	the	DET
ap-8157	127	18	propulsion	propulsion	NOUN
ap-8157	127	19	system	system	NOUN
ap-8157	127	20	for	for	ADP
ap-8157	127	21	different	different	ADJ
ap-8157	127	22	fan	fan	NOUN
ap-8157	127	23	diameters	diameter	NOUN
ap-8157	127	24	d1	d1	NOUN
ap-8157	127	25	,	,	PUNCT
ap-8157	127	26	nozzle	nozzle	NOUN
ap-8157	127	27	contraction	contraction	NOUN
ap-8157	127	28	ratio	ratio	NOUN
ap-8157	127	29	a1	a1	PROPN
ap-8157	127	30	/	/	SYM
ap-8157	127	31	a3	a3	NOUN
ap-8157	127	32	=	=	SYM
ap-8157	127	33	1	1	X
ap-8157	127	34	.	.	X
ap-8157	127	35	figure	figure	NOUN
ap-8157	127	36	5	5	NUM
ap-8157	127	37	.	.	PUNCT
ap-8157	127	38	efficiency	efficiency	NOUN
ap-8157	127	39	of	of	ADP
ap-8157	127	40	the	the	DET
ap-8157	127	41	propulsion	propulsion	NOUN
ap-8157	127	42	system	system	NOUN
ap-8157	127	43	for	for	ADP
ap-8157	127	44	different	different	ADJ
ap-8157	127	45	nozzle	nozzle	NOUN
ap-8157	127	46	contraction	contraction	NOUN
ap-8157	127	47	a1	a1	NOUN
ap-8157	127	48	/	/	SYM
ap-8157	127	49	a3	a3	NOUN
ap-8157	127	50	,	,	PUNCT
ap-8157	128	1	fan	fan	NOUN
ap-8157	128	2	diameter	diameter	NOUN
ap-8157	128	3	d1	d1	PROPN
ap-8157	128	4	=	=	PROPN
ap-8157	128	5	0.66	0.66	NUM
ap-8157	128	6	m.	m.	NOUN
ap-8157	128	7	figure	figure	NOUN
ap-8157	128	8	6	6	NUM
ap-8157	128	9	.	.	PUNCT
ap-8157	129	1	fan	fan	PROPN
ap-8157	129	2	axial	axial	ADJ
ap-8157	129	3	velocity	velocity	NOUN
ap-8157	129	4	component	component	NOUN
ap-8157	129	5	over	over	ADP
ap-8157	129	6	flight	flight	NOUN
ap-8157	129	7	speed	speed	NOUN
ap-8157	129	8	for	for	ADP
ap-8157	129	9	different	different	ADJ
ap-8157	129	10	fan	fan	NOUN
ap-8157	129	11	diamenters	diamenter	NOUN
ap-8157	129	12	and	and	CCONJ
ap-8157	129	13	a1	a1	NOUN
ap-8157	129	14	/	/	SYM
ap-8157	129	15	a3	a3	NOUN
ap-8157	129	16	=	=	SYM
ap-8157	129	17	1	1	X
ap-8157	129	18	.	.	X
ap-8157	129	19	figure	figure	VERB
ap-8157	129	20	7	7	NUM
ap-8157	129	21	.	.	PUNCT
ap-8157	129	22	fan	fan	PROPN
ap-8157	129	23	axial	axial	ADJ
ap-8157	129	24	velocity	velocity	NOUN
ap-8157	129	25	component	component	NOUN
ap-8157	129	26	over	over	ADP
ap-8157	129	27	flight	flight	NOUN
ap-8157	129	28	speed	speed	NOUN
ap-8157	129	29	for	for	ADP
ap-8157	129	30	different	different	ADJ
ap-8157	129	31	nozzle	nozzle	NOUN
ap-8157	129	32	contraction	contraction	NOUN
ap-8157	129	33	ratios	ratio	VERB
ap-8157	129	34	a1	a1	NOUN
ap-8157	129	35	/	/	SYM
ap-8157	129	36	a3	a3	NOUN
ap-8157	129	37	,	,	PUNCT
ap-8157	129	38	fan	fan	NOUN
ap-8157	129	39	diameter	diameter	NOUN
ap-8157	129	40	d1	d1	PROPN
ap-8157	129	41	=	=	PROPN
ap-8157	129	42	0.66	0.66	NUM
ap-8157	129	43	m.	m.	NOUN
ap-8157	129	44	figure	figure	NOUN
ap-8157	129	45	8	8	NUM
ap-8157	129	46	.	.	PUNCT
ap-8157	130	1	fan	fan	NOUN
ap-8157	130	2	pressure	pressure	NOUN
ap-8157	130	3	ratio	ratio	NOUN
ap-8157	130	4	over	over	ADP
ap-8157	130	5	flight	flight	NOUN
ap-8157	130	6	speed	speed	NOUN
ap-8157	130	7	for	for	ADP
ap-8157	130	8	different	different	ADJ
ap-8157	130	9	fan	fan	NOUN
ap-8157	130	10	diamenters	diamenter	NOUN
ap-8157	130	11	and	and	CCONJ
ap-8157	130	12	a1	a1	NOUN
ap-8157	130	13	/	/	SYM
ap-8157	130	14	a3	a3	NOUN
ap-8157	130	15	=	=	SYM
ap-8157	130	16	1	1	X
ap-8157	130	17	.	.	X
ap-8157	130	18	figure	figure	NOUN
ap-8157	130	19	9	9	NUM
ap-8157	130	20	.	.	PUNCT
ap-8157	131	1	fan	fan	PROPN
ap-8157	131	2	rpm	rpm	PROPN
ap-8157	131	3	over	over	ADP
ap-8157	131	4	flight	flight	NOUN
ap-8157	131	5	speed	speed	NOUN
ap-8157	131	6	for	for	ADP
ap-8157	131	7	different	different	ADJ
ap-8157	131	8	fan	fan	NOUN
ap-8157	131	9	diamenters	diamenter	NOUN
ap-8157	131	10	and	and	CCONJ
ap-8157	131	11	a1	a1	NOUN
ap-8157	131	12	/	/	SYM
ap-8157	131	13	a3	a3	NOUN
ap-8157	131	14	=	=	SYM
ap-8157	131	15	1	1	NUM
ap-8157	131	16	.	.	NUM
ap-8157	131	17	553	553	NUM
ap-8157	131	18	jan	jan	PROPN
ap-8157	131	19	klesa	klesa	PROPN
ap-8157	131	20	acta	acta	PROPN
ap-8157	131	21	polytechnica	polytechnica	PROPN
ap-8157	131	22	figure	figure	NOUN
ap-8157	131	23	10	10	NUM
ap-8157	131	24	.	.	PUNCT
ap-8157	132	1	dependence	dependence	NOUN
ap-8157	132	2	of	of	ADP
ap-8157	132	3	static	static	PROPN
ap-8157	132	4	thrust	thrust	NOUN
ap-8157	132	5	on	on	ADP
ap-8157	132	6	fan	fan	NOUN
ap-8157	132	7	diameter	diameter	NOUN
ap-8157	132	8	and	and	CCONJ
ap-8157	132	9	nozzle	nozzle	NOUN
ap-8157	132	10	contraction	contraction	NOUN
ap-8157	132	11	ratio	ratio	NOUN
ap-8157	132	12	a1	a1	PROPN
ap-8157	132	13	/	/	SYM
ap-8157	132	14	a3	a3	NOUN
ap-8157	132	15	.	.	PUNCT
ap-8157	133	1	the	the	DET
ap-8157	133	2	selected	select	VERB
ap-8157	133	3	fan	fan	NOUN
ap-8157	133	4	design	design	NOUN
ap-8157	133	5	point	point	NOUN
ap-8157	133	6	parameters	parameter	NOUN
ap-8157	133	7	are	be	AUX
ap-8157	133	8	marked	mark	VERB
ap-8157	133	9	by	by	ADP
ap-8157	133	10	red	red	PROPN
ap-8157	133	11	cross	cross	PROPN
ap-8157	133	12	.	.	PROPN
ap-8157	134	1	figure	figure	NOUN
ap-8157	134	2	11	11	NUM
ap-8157	134	3	.	.	PUNCT
ap-8157	135	1	dependence	dependence	NOUN
ap-8157	135	2	of	of	ADP
ap-8157	135	3	thrust	thrust	NOUN
ap-8157	135	4	at	at	ADP
ap-8157	135	5	flight	flight	NOUN
ap-8157	135	6	speed	speed	NOUN
ap-8157	135	7	v0	v0	NOUN
ap-8157	135	8	=	=	SYM
ap-8157	135	9	300	300	NUM
ap-8157	135	10	km	km	NOUN
ap-8157	135	11	h−1	h−1	PROPN
ap-8157	135	12	on	on	ADP
ap-8157	135	13	fan	fan	NOUN
ap-8157	135	14	diameter	diameter	NOUN
ap-8157	135	15	and	and	CCONJ
ap-8157	135	16	nozzle	nozzle	NOUN
ap-8157	135	17	contraction	contraction	NOUN
ap-8157	135	18	ratio	ratio	NOUN
ap-8157	135	19	a1	a1	PROPN
ap-8157	135	20	/	/	SYM
ap-8157	135	21	a3	a3	NOUN
ap-8157	135	22	.	.	PUNCT
ap-8157	136	1	the	the	DET
ap-8157	136	2	selected	select	VERB
ap-8157	136	3	fan	fan	NOUN
ap-8157	136	4	design	design	NOUN
ap-8157	136	5	point	point	NOUN
ap-8157	136	6	parameters	parameter	NOUN
ap-8157	136	7	are	be	AUX
ap-8157	136	8	marked	mark	VERB
ap-8157	136	9	by	by	ADP
ap-8157	136	10	red	red	PROPN
ap-8157	136	11	cross	cross	PROPN
ap-8157	136	12	.	.	PROPN
ap-8157	137	1	figure	figure	NOUN
ap-8157	137	2	12	12	NUM
ap-8157	137	3	.	.	PUNCT
ap-8157	138	1	dependence	dependence	NOUN
ap-8157	138	2	of	of	ADP
ap-8157	138	3	fan	fan	NOUN
ap-8157	138	4	pressure	pressure	NOUN
ap-8157	138	5	ratio	ratio	NOUN
ap-8157	138	6	at	at	ADP
ap-8157	138	7	flight	flight	NOUN
ap-8157	138	8	speed	speed	NOUN
ap-8157	138	9	v0	v0	NOUN
ap-8157	138	10	=	=	SYM
ap-8157	138	11	0	0	NUM
ap-8157	138	12	km	km	NOUN
ap-8157	138	13	h−1	h−1	PROPN
ap-8157	138	14	on	on	ADP
ap-8157	138	15	fan	fan	NOUN
ap-8157	138	16	diameter	diameter	NOUN
ap-8157	138	17	and	and	CCONJ
ap-8157	138	18	nozzle	nozzle	NOUN
ap-8157	138	19	contraction	contraction	NOUN
ap-8157	138	20	ratio	ratio	NOUN
ap-8157	138	21	a1	a1	PROPN
ap-8157	138	22	/	/	SYM
ap-8157	138	23	a3	a3	NOUN
ap-8157	138	24	.	.	PUNCT
ap-8157	139	1	the	the	DET
ap-8157	139	2	selected	select	VERB
ap-8157	139	3	fan	fan	NOUN
ap-8157	139	4	design	design	NOUN
ap-8157	139	5	point	point	NOUN
ap-8157	139	6	parameters	parameter	NOUN
ap-8157	139	7	are	be	AUX
ap-8157	139	8	marked	mark	VERB
ap-8157	139	9	by	by	ADP
ap-8157	139	10	red	red	PROPN
ap-8157	139	11	cross	cross	PROPN
ap-8157	139	12	.	.	PROPN
ap-8157	140	1	figure	figure	NOUN
ap-8157	140	2	13	13	NUM
ap-8157	140	3	.	.	PUNCT
ap-8157	141	1	dependence	dependence	NOUN
ap-8157	141	2	of	of	ADP
ap-8157	141	3	fan	fan	NOUN
ap-8157	141	4	pressure	pressure	NOUN
ap-8157	141	5	ratio	ratio	NOUN
ap-8157	141	6	at	at	ADP
ap-8157	141	7	flight	flight	NOUN
ap-8157	141	8	speed	speed	NOUN
ap-8157	141	9	v0	v0	NOUN
ap-8157	141	10	=	=	SYM
ap-8157	141	11	300	300	NUM
ap-8157	141	12	km	km	NOUN
ap-8157	141	13	h−1	h−1	PROPN
ap-8157	141	14	on	on	ADP
ap-8157	141	15	fan	fan	NOUN
ap-8157	141	16	diameter	diameter	NOUN
ap-8157	141	17	and	and	CCONJ
ap-8157	141	18	nozzle	nozzle	NOUN
ap-8157	141	19	contraction	contraction	NOUN
ap-8157	141	20	ratio	ratio	NOUN
ap-8157	141	21	a1	a1	PROPN
ap-8157	141	22	/	/	SYM
ap-8157	141	23	a3	a3	NOUN
ap-8157	141	24	.	.	PUNCT
ap-8157	142	1	the	the	DET
ap-8157	142	2	selected	select	VERB
ap-8157	142	3	fan	fan	NOUN
ap-8157	142	4	design	design	NOUN
ap-8157	142	5	point	point	NOUN
ap-8157	142	6	parameters	parameter	NOUN
ap-8157	142	7	are	be	AUX
ap-8157	142	8	marked	mark	VERB
ap-8157	142	9	by	by	ADP
ap-8157	142	10	red	red	PROPN
ap-8157	142	11	cross	cross	PROPN
ap-8157	142	12	.	.	PUNCT
ap-8157	143	1	the	the	DET
ap-8157	143	2	maximum	maximum	PROPN
ap-8157	143	3	thrust	thrust	NOUN
ap-8157	143	4	for	for	ADP
ap-8157	143	5	each	each	DET
ap-8157	143	6	velocity	velocity	NOUN
ap-8157	143	7	.	.	PUNCT
ap-8157	144	1	the	the	DET
ap-8157	144	2	optimal	optimal	ADJ
ap-8157	144	3	value	value	NOUN
ap-8157	144	4	is	be	AUX
ap-8157	144	5	the	the	DET
ap-8157	144	6	maximum	maximum	NOUN
ap-8157	144	7	of	of	ADP
ap-8157	144	8	relative	relative	ADJ
ap-8157	144	9	thrust	thrust	NOUN
ap-8157	144	10	mean	mean	ADJ
ap-8157	144	11	value	value	NOUN
ap-8157	144	12	for	for	ADP
ap-8157	144	13	flight	flight	NOUN
ap-8157	144	14	velocity	velocity	NOUN
ap-8157	144	15	0	0	NUM
ap-8157	144	16	km	km	NOUN
ap-8157	145	1	h−1	h−1	PROPN
ap-8157	145	2	and	and	CCONJ
ap-8157	145	3	300	300	NUM
ap-8157	145	4	km	km	NOUN
ap-8157	145	5	h−1	h−1	PROPN
ap-8157	145	6	.	.	PUNCT
ap-8157	146	1	this	this	PRON
ap-8157	146	2	gives	give	VERB
ap-8157	146	3	an	an	DET
ap-8157	146	4	optimal	optimal	ADJ
ap-8157	146	5	value	value	NOUN
ap-8157	146	6	of	of	ADP
ap-8157	146	7	a1	a1	NOUN
ap-8157	146	8	/	/	SYM
ap-8157	146	9	a3	a3	NOUN
ap-8157	146	10	equal	equal	ADJ
ap-8157	146	11	to	to	ADP
ap-8157	146	12	1.17	1.17	NUM
ap-8157	146	13	.	.	PUNCT
ap-8157	147	1	the	the	DET
ap-8157	147	2	resulting	result	VERB
ap-8157	147	3	performance	performance	NOUN
ap-8157	147	4	of	of	ADP
ap-8157	147	5	the	the	DET
ap-8157	147	6	propulsion	propulsion	NOUN
ap-8157	147	7	system	system	NOUN
ap-8157	147	8	is	be	AUX
ap-8157	147	9	then	then	ADV
ap-8157	147	10	determined	determined	ADJ
ap-8157	147	11	for	for	ADP
ap-8157	147	12	this	this	DET
ap-8157	147	13	case	case	NOUN
ap-8157	147	14	,	,	PUNCT
ap-8157	147	15	see	see	VERB
ap-8157	147	16	figures	figure	NOUN
ap-8157	147	17	19	19	NUM
ap-8157	147	18	and	and	CCONJ
ap-8157	147	19	20	20	NUM
ap-8157	147	20	.	.	PUNCT
ap-8157	148	1	also	also	ADV
ap-8157	148	2	,	,	PUNCT
ap-8157	148	3	the	the	DET
ap-8157	148	4	dependence	dependence	NOUN
ap-8157	148	5	of	of	ADP
ap-8157	148	6	the	the	DET
ap-8157	148	7	fan	fan	NOUN
ap-8157	148	8	design	design	NOUN
ap-8157	148	9	parameters	parameter	NOUN
ap-8157	148	10	on	on	ADP
ap-8157	148	11	the	the	DET
ap-8157	148	12	flight	flight	NOUN
ap-8157	148	13	velocity	velocity	NOUN
ap-8157	148	14	is	be	AUX
ap-8157	148	15	computed	compute	VERB
ap-8157	148	16	,	,	PUNCT
ap-8157	148	17	i.e.	i.e.	X
ap-8157	148	18	fan	fan	NOUN
ap-8157	148	19	pressure	pressure	NOUN
ap-8157	148	20	ratio	ratio	NOUN
ap-8157	148	21	π	π	PROPN
ap-8157	148	22	in	in	ADP
ap-8157	148	23	figure	figure	NOUN
ap-8157	148	24	21	21	NUM
ap-8157	148	25	,	,	PUNCT
ap-8157	148	26	fan	fan	PROPN
ap-8157	148	27	axial	axial	ADJ
ap-8157	148	28	velocity	velocity	NOUN
ap-8157	148	29	v0	v0	NOUN
ap-8157	148	30	in	in	ADP
ap-8157	148	31	figure	figure	NOUN
ap-8157	148	32	22	22	NUM
ap-8157	148	33	and	and	CCONJ
ap-8157	148	34	fan	fan	PROPN
ap-8157	148	35	rpm	rpm	PROPN
ap-8157	148	36	nm	nm	PROPN
ap-8157	148	37	in	in	ADP
ap-8157	148	38	figure	figure	NOUN
ap-8157	148	39	23	23	NUM
ap-8157	148	40	.	.	PUNCT
ap-8157	149	1	4	4	X
ap-8157	149	2	.	.	X
ap-8157	149	3	discussion	discussion	NOUN
ap-8157	149	4	the	the	DET
ap-8157	149	5	presented	present	VERB
ap-8157	149	6	results	result	NOUN
ap-8157	149	7	show	show	VERB
ap-8157	149	8	that	that	SCONJ
ap-8157	149	9	the	the	DET
ap-8157	149	10	high	high	ADJ
ap-8157	149	11	static	static	ADJ
ap-8157	149	12	thrust	thrust	NOUN
ap-8157	149	13	requirement	requirement	NOUN
ap-8157	149	14	is	be	AUX
ap-8157	149	15	in	in	ADP
ap-8157	149	16	conflict	conflict	NOUN
ap-8157	149	17	with	with	ADP
ap-8157	149	18	the	the	DET
ap-8157	149	19	high	high	ADJ
ap-8157	149	20	cruise	cruise	NOUN
ap-8157	149	21	speed	speed	NOUN
ap-8157	149	22	requirement	requirement	NOUN
ap-8157	149	23	(	(	PUNCT
ap-8157	149	24	i.e.	i.e.	X
ap-8157	149	25	high	high	ADJ
ap-8157	149	26	thrust	thrust	NOUN
ap-8157	149	27	at	at	ADP
ap-8157	149	28	high	high	ADJ
ap-8157	149	29	flight	flight	NOUN
ap-8157	149	30	velocity	velocity	NOUN
ap-8157	149	31	)	)	PUNCT
ap-8157	149	32	as	as	SCONJ
ap-8157	149	33	expected	expect	VERB
ap-8157	149	34	from	from	ADP
ap-8157	149	35	the	the	DET
ap-8157	149	36	general	general	ADJ
ap-8157	149	37	aircraft	aircraft	NOUN
ap-8157	149	38	propulsion	propulsion	NOUN
ap-8157	149	39	theory	theory	NOUN
ap-8157	149	40	.	.	PUNCT
ap-8157	150	1	this	this	PRON
ap-8157	150	2	is	be	AUX
ap-8157	150	3	clearly	clearly	ADV
ap-8157	150	4	visible	visible	ADJ
ap-8157	150	5	in	in	ADP
ap-8157	150	6	figure	figure	NOUN
ap-8157	150	7	18	18	NUM
ap-8157	150	8	.	.	PUNCT
ap-8157	151	1	the	the	DET
ap-8157	151	2	ul-39	ul-39	ADJ
ap-8157	151	3	light	light	ADJ
ap-8157	151	4	-	-	PUNCT
ap-8157	151	5	sport	sport	NOUN
ap-8157	151	6	aircraft	aircraft	NOUN
ap-8157	151	7	is	be	AUX
ap-8157	151	8	used	use	VERB
ap-8157	151	9	as	as	ADP
ap-8157	151	10	an	an	DET
ap-8157	151	11	example	example	NOUN
ap-8157	151	12	for	for	ADP
ap-8157	151	13	this	this	DET
ap-8157	151	14	computation	computation	NOUN
ap-8157	151	15	;	;	PUNCT
ap-8157	151	16	the	the	DET
ap-8157	151	17	results	result	NOUN
ap-8157	151	18	for	for	ADP
ap-8157	151	19	similar	similar	ADJ
ap-8157	151	20	aircrafts	aircraft	NOUN
ap-8157	151	21	are	be	AUX
ap-8157	151	22	expected	expect	VERB
ap-8157	151	23	to	to	PART
ap-8157	151	24	be	be	AUX
ap-8157	151	25	comparable	comparable	ADJ
ap-8157	151	26	.	.	PUNCT
ap-8157	152	1	that	that	PRON
ap-8157	152	2	is	be	AUX
ap-8157	152	3	why	why	SCONJ
ap-8157	152	4	the	the	DET
ap-8157	152	5	optimal	optimal	ADJ
ap-8157	152	6	system	system	NOUN
ap-8157	152	7	configuration	configuration	NOUN
ap-8157	152	8	is	be	AUX
ap-8157	152	9	set	set	VERB
ap-8157	152	10	by	by	ADP
ap-8157	152	11	means	mean	NOUN
ap-8157	152	12	of	of	ADP
ap-8157	152	13	relative	relative	ADJ
ap-8157	152	14	thrust	thrust	PROPN
ap-8157	152	15	.	.	PUNCT
ap-8157	153	1	the	the	DET
ap-8157	153	2	outputs	output	NOUN
ap-8157	153	3	of	of	ADP
ap-8157	153	4	this	this	DET
ap-8157	153	5	method	method	NOUN
ap-8157	153	6	are	be	AUX
ap-8157	153	7	the	the	DET
ap-8157	153	8	fan	fan	PROPN
ap-8157	153	9	design	design	NOUN
ap-8157	153	10	parameters	parameter	NOUN
ap-8157	153	11	presented	present	VERB
ap-8157	153	12	in	in	ADP
ap-8157	153	13	table	table	NOUN
ap-8157	153	14	3	3	NUM
ap-8157	153	15	.	.	NOUN
ap-8157	153	16	5	5	NUM
ap-8157	153	17	.	.	PUNCT
ap-8157	153	18	conclusions	conclusion	NOUN
ap-8157	153	19	the	the	DET
ap-8157	153	20	results	result	NOUN
ap-8157	153	21	of	of	ADP
ap-8157	153	22	the	the	DET
ap-8157	153	23	propulsion	propulsion	NOUN
ap-8157	153	24	system	system	NOUN
ap-8157	153	25	simulation	simulation	NOUN
ap-8157	153	26	for	for	ADP
ap-8157	153	27	ducted	ducte	VERB
ap-8157	153	28	fan	fan	NOUN
ap-8157	153	29	aircraft	aircraft	NOUN
ap-8157	153	30	are	be	AUX
ap-8157	153	31	presented	present	VERB
ap-8157	153	32	.	.	PUNCT
ap-8157	154	1	a	a	DET
ap-8157	154	2	compressible	compressible	ADJ
ap-8157	154	3	fluid	fluid	NOUN
ap-8157	154	4	flow	flow	NOUN
ap-8157	154	5	model	model	NOUN
ap-8157	154	6	is	be	AUX
ap-8157	154	7	used	use	VERB
ap-8157	154	8	so	so	SCONJ
ap-8157	154	9	the	the	DET
ap-8157	154	10	described	describe	VERB
ap-8157	154	11	procedure	procedure	NOUN
ap-8157	154	12	can	can	AUX
ap-8157	154	13	be	be	AUX
ap-8157	154	14	used	use	VERB
ap-8157	154	15	for	for	ADP
ap-8157	154	16	a	a	DET
ap-8157	154	17	wider	wide	ADJ
ap-8157	154	18	range	range	NOUN
ap-8157	154	19	of	of	ADP
ap-8157	154	20	flight	flight	NOUN
ap-8157	154	21	velocities	velocity	NOUN
ap-8157	154	22	in	in	ADP
ap-8157	154	23	comparison	comparison	NOUN
ap-8157	154	24	with	with	ADP
ap-8157	154	25	a	a	DET
ap-8157	154	26	simple	simple	ADJ
ap-8157	154	27	,	,	PUNCT
ap-8157	154	28	incompressible	incompressible	ADJ
ap-8157	154	29	flow	flow	NOUN
ap-8157	154	30	model	model	NOUN
ap-8157	154	31	(	(	PUNCT
ap-8157	154	32	e.g.	e.g.	ADV
ap-8157	154	33	[	[	X
ap-8157	154	34	4	4	NUM
ap-8157	154	35	]	]	NUM
ap-8157	154	36	)	)	PUNCT
ap-8157	154	37	.	.	PUNCT
ap-8157	155	1	the	the	DET
ap-8157	155	2	procedure	procedure	NOUN
ap-8157	155	3	is	be	AUX
ap-8157	155	4	described	describe	VERB
ap-8157	155	5	and	and	CCONJ
ap-8157	155	6	results	result	NOUN
ap-8157	155	7	are	be	AUX
ap-8157	155	8	presented	present	VERB
ap-8157	155	9	for	for	ADP
ap-8157	155	10	the	the	DET
ap-8157	155	11	example	example	NOUN
ap-8157	155	12	of	of	ADP
ap-8157	155	13	the	the	DET
ap-8157	155	14	ul-39	ul-39	ADJ
ap-8157	155	15	aircraft	aircraft	NOUN
ap-8157	155	16	.	.	PUNCT
ap-8157	156	1	the	the	DET
ap-8157	156	2	requirements	requirement	NOUN
ap-8157	156	3	for	for	ADP
ap-8157	156	4	the	the	DET
ap-8157	156	5	propulsion	propulsion	NOUN
ap-8157	156	6	system	system	NOUN
ap-8157	156	7	are	be	AUX
ap-8157	156	8	contradictory	contradictory	ADJ
ap-8157	156	9	,	,	PUNCT
ap-8157	156	10	i.e.	i.e.	X
ap-8157	156	11	short	short	ADJ
ap-8157	156	12	take	take	VERB
ap-8157	156	13	-	-	PUNCT
ap-8157	156	14	off	off	NOUN
ap-8157	156	15	distance	distance	NOUN
ap-8157	156	16	and	and	CCONJ
ap-8157	156	17	high	high	ADJ
ap-8157	156	18	maximal	maximal	ADJ
ap-8157	156	19	554	554	NUM
ap-8157	156	20	vol	vol	NOUN
ap-8157	156	21	.	.	PUNCT
ap-8157	157	1	62	62	NUM
ap-8157	157	2	no	no	INTJ
ap-8157	157	3	.	.	PUNCT
ap-8157	158	1	5/2022	5/2022	NOUN
ap-8157	158	2	determination	determination	NOUN
ap-8157	158	3	of	of	ADP
ap-8157	158	4	fan	fan	NOUN
ap-8157	158	5	design	design	NOUN
ap-8157	158	6	parameters	parameter	NOUN
ap-8157	158	7	for	for	ADP
ap-8157	158	8	light	light	ADJ
ap-8157	158	9	-	-	PUNCT
ap-8157	158	10	sport	sport	NOUN
ap-8157	158	11	aircraft	aircraft	NOUN
ap-8157	158	12	figure	figure	NOUN
ap-8157	158	13	14	14	NUM
ap-8157	158	14	.	.	PUNCT
ap-8157	159	1	dependence	dependence	NOUN
ap-8157	159	2	of	of	ADP
ap-8157	159	3	fan	fan	PROPN
ap-8157	159	4	axial	axial	ADJ
ap-8157	159	5	velocity	velocity	NOUN
ap-8157	159	6	component	component	NOUN
ap-8157	159	7	at	at	ADP
ap-8157	159	8	flight	flight	NOUN
ap-8157	159	9	speed	speed	NOUN
ap-8157	159	10	v0	v0	NOUN
ap-8157	159	11	=	=	SYM
ap-8157	159	12	0	0	NUM
ap-8157	159	13	km	km	NOUN
ap-8157	159	14	h−1	h−1	PROPN
ap-8157	159	15	on	on	ADP
ap-8157	159	16	fan	fan	NOUN
ap-8157	159	17	diameter	diameter	NOUN
ap-8157	159	18	and	and	CCONJ
ap-8157	159	19	nozzle	nozzle	NOUN
ap-8157	159	20	contraction	contraction	NOUN
ap-8157	159	21	ratio	ratio	NOUN
ap-8157	159	22	a1	a1	PROPN
ap-8157	159	23	/	/	SYM
ap-8157	159	24	a3	a3	NOUN
ap-8157	159	25	.	.	PUNCT
ap-8157	160	1	the	the	DET
ap-8157	160	2	selected	select	VERB
ap-8157	160	3	fan	fan	NOUN
ap-8157	160	4	design	design	NOUN
ap-8157	160	5	point	point	NOUN
ap-8157	160	6	parameters	parameter	NOUN
ap-8157	160	7	are	be	AUX
ap-8157	160	8	marked	mark	VERB
ap-8157	160	9	by	by	ADP
ap-8157	160	10	red	red	PROPN
ap-8157	160	11	cross	cross	PROPN
ap-8157	160	12	.	.	PROPN
ap-8157	161	1	figure	figure	NOUN
ap-8157	161	2	15	15	NUM
ap-8157	161	3	.	.	PUNCT
ap-8157	162	1	dependence	dependence	NOUN
ap-8157	162	2	of	of	ADP
ap-8157	162	3	fan	fan	PROPN
ap-8157	162	4	axial	axial	ADJ
ap-8157	162	5	velocity	velocity	NOUN
ap-8157	162	6	component	component	NOUN
ap-8157	162	7	at	at	ADP
ap-8157	162	8	flight	flight	NOUN
ap-8157	162	9	speed	speed	NOUN
ap-8157	162	10	v0	v0	NOUN
ap-8157	162	11	=	=	SYM
ap-8157	162	12	300	300	NUM
ap-8157	162	13	km	km	NOUN
ap-8157	162	14	h−1	h−1	PROPN
ap-8157	162	15	on	on	ADP
ap-8157	162	16	fan	fan	NOUN
ap-8157	162	17	diameter	diameter	NOUN
ap-8157	162	18	and	and	CCONJ
ap-8157	162	19	nozzle	nozzle	NOUN
ap-8157	162	20	contraction	contraction	NOUN
ap-8157	162	21	ratio	ratio	NOUN
ap-8157	162	22	a1	a1	PROPN
ap-8157	162	23	/	/	SYM
ap-8157	162	24	a3	a3	NOUN
ap-8157	162	25	.	.	PUNCT
ap-8157	163	1	the	the	DET
ap-8157	163	2	selected	select	VERB
ap-8157	163	3	fan	fan	NOUN
ap-8157	163	4	design	design	NOUN
ap-8157	163	5	point	point	NOUN
ap-8157	163	6	parameters	parameter	NOUN
ap-8157	163	7	are	be	AUX
ap-8157	163	8	marked	mark	VERB
ap-8157	163	9	by	by	ADP
ap-8157	163	10	red	red	PROPN
ap-8157	163	11	cross	cross	PROPN
ap-8157	163	12	.	.	PROPN
ap-8157	164	1	figure	figure	NOUN
ap-8157	164	2	16	16	NUM
ap-8157	164	3	.	.	PUNCT
ap-8157	165	1	dependence	dependence	NOUN
ap-8157	165	2	of	of	ADP
ap-8157	165	3	fan	fan	PROPN
ap-8157	165	4	rpm	rpm	NOUN
ap-8157	165	5	at	at	ADP
ap-8157	165	6	flight	flight	NOUN
ap-8157	165	7	speed	speed	NOUN
ap-8157	165	8	v0	v0	NOUN
ap-8157	165	9	=	=	SYM
ap-8157	165	10	0	0	NUM
ap-8157	165	11	km	km	NOUN
ap-8157	165	12	h−1	h−1	PROPN
ap-8157	165	13	on	on	ADP
ap-8157	165	14	fan	fan	NOUN
ap-8157	165	15	diameter	diameter	NOUN
ap-8157	165	16	and	and	CCONJ
ap-8157	165	17	nozzle	nozzle	NOUN
ap-8157	165	18	contraction	contraction	NOUN
ap-8157	165	19	ratio	ratio	NOUN
ap-8157	165	20	a1	a1	PROPN
ap-8157	165	21	/	/	SYM
ap-8157	165	22	a3	a3	NOUN
ap-8157	165	23	.	.	PUNCT
ap-8157	166	1	the	the	DET
ap-8157	166	2	selected	select	VERB
ap-8157	166	3	fan	fan	NOUN
ap-8157	166	4	design	design	NOUN
ap-8157	166	5	point	point	NOUN
ap-8157	166	6	are	be	AUX
ap-8157	166	7	marked	mark	VERB
ap-8157	166	8	by	by	ADP
ap-8157	166	9	red	red	PROPN
ap-8157	166	10	cross	cross	PROPN
ap-8157	166	11	.	.	PROPN
ap-8157	167	1	figure	figure	NOUN
ap-8157	167	2	17	17	NUM
ap-8157	167	3	.	.	PUNCT
ap-8157	168	1	dependence	dependence	NOUN
ap-8157	168	2	of	of	ADP
ap-8157	168	3	fan	fan	PROPN
ap-8157	168	4	rpm	rpm	NOUN
ap-8157	168	5	at	at	ADP
ap-8157	168	6	flight	flight	NOUN
ap-8157	168	7	speed	speed	NOUN
ap-8157	168	8	v0	v0	NOUN
ap-8157	168	9	=	=	SYM
ap-8157	168	10	300	300	NUM
ap-8157	168	11	km	km	NOUN
ap-8157	168	12	h−1	h−1	PROPN
ap-8157	168	13	on	on	ADP
ap-8157	168	14	fan	fan	NOUN
ap-8157	168	15	diameter	diameter	NOUN
ap-8157	168	16	and	and	CCONJ
ap-8157	168	17	nozzle	nozzle	NOUN
ap-8157	168	18	contraction	contraction	NOUN
ap-8157	168	19	ratio	ratio	NOUN
ap-8157	168	20	a1	a1	PROPN
ap-8157	168	21	/	/	SYM
ap-8157	168	22	a3	a3	NOUN
ap-8157	168	23	.	.	PUNCT
ap-8157	169	1	the	the	DET
ap-8157	169	2	selected	select	VERB
ap-8157	169	3	fan	fan	NOUN
ap-8157	169	4	design	design	NOUN
ap-8157	169	5	point	point	NOUN
ap-8157	169	6	parameters	parameter	NOUN
ap-8157	169	7	are	be	AUX
ap-8157	169	8	marked	mark	VERB
ap-8157	169	9	by	by	ADP
ap-8157	169	10	red	red	PROPN
ap-8157	169	11	cross	cross	PROPN
ap-8157	169	12	.	.	PUNCT
ap-8157	170	1	fan	fan	PROPN
ap-8157	170	2	pressure	pressure	NOUN
ap-8157	170	3	ratio	ratio	NOUN
ap-8157	170	4	π	π	PROPN
ap-8157	170	5	1.062	1.062	NUM
ap-8157	170	6	fan	fan	NOUN
ap-8157	170	7	diameter	diameter	NOUN
ap-8157	171	1	d	d	ADP
ap-8157	171	2	660	660	NUM
ap-8157	171	3	mm	mm	NOUN
ap-8157	171	4	electric	electric	PROPN
ap-8157	171	5	motor	motor	PROPN
ap-8157	171	6	rpm	rpm	PROPN
ap-8157	171	7	6340	6340	NUM
ap-8157	171	8	air	air	NOUN
ap-8157	171	9	axial	axial	ADJ
ap-8157	171	10	velocity	velocity	NOUN
ap-8157	171	11	at	at	ADP
ap-8157	171	12	fan	fan	PROPN
ap-8157	171	13	vax	vax	PROPN
ap-8157	171	14	109.54	109.54	NUM
ap-8157	171	15	m	m	VERB
ap-8157	171	16	s−1	s−1	PROPN
ap-8157	171	17	fan	fan	PROPN
ap-8157	171	18	air	air	PROPN
ap-8157	171	19	mass	mass	PROPN
ap-8157	171	20	flow	flow	NOUN
ap-8157	171	21	ṁ	ṁ	PROPN
ap-8157	171	22	33.46	33.46	NUM
ap-8157	171	23	kg	kg	NOUN
ap-8157	172	1	s−1	s−1	PROPN
ap-8157	172	2	expected	expect	VERB
ap-8157	172	3	thrust	thrust	VERB
ap-8157	172	4	at	at	ADP
ap-8157	172	5	300	300	NUM
ap-8157	172	6	km	km	NOUN
ap-8157	173	1	h−1	h−1	PROPN
ap-8157	173	2	t	t	PROPN
ap-8157	173	3	1401.9	1401.9	NUM
ap-8157	173	4	n	n	PRON
ap-8157	173	5	expected	expect	VERB
ap-8157	173	6	efficiency	efficiency	NOUN
ap-8157	173	7	at	at	ADP
ap-8157	173	8	300	300	NUM
ap-8157	173	9	km	km	NOUN
ap-8157	173	10	h−1	h−1	PROPN
ap-8157	173	11	η	η	NOUN
ap-8157	173	12	0.584	0.584	NUM
ap-8157	173	13	table	table	NOUN
ap-8157	173	14	3	3	NUM
ap-8157	173	15	.	.	PUNCT
ap-8157	173	16	ul-39	ul-39	PROPN
ap-8157	173	17	fan	fan	PROPN
ap-8157	173	18	design	design	NOUN
ap-8157	173	19	parameters	parameter	NOUN
ap-8157	173	20	for	for	ADP
ap-8157	173	21	flight	flight	NOUN
ap-8157	173	22	speed	speed	NOUN
ap-8157	173	23	300	300	NUM
ap-8157	173	24	km	km	NOUN
ap-8157	173	25	h−1	h−1	PROPN
ap-8157	173	26	at	at	ADP
ap-8157	173	27	sea	sea	NOUN
ap-8157	173	28	level	level	NOUN
ap-8157	173	29	international	international	ADJ
ap-8157	173	30	standard	standard	ADJ
ap-8157	173	31	atmosphere	atmosphere	NOUN
ap-8157	173	32	and	and	CCONJ
ap-8157	173	33	electric	electric	ADJ
ap-8157	173	34	motor	motor	NOUN
ap-8157	173	35	power	power	NOUN
ap-8157	173	36	200	200	NUM
ap-8157	173	37	kw	kw	NOUN
ap-8157	173	38	.	.	PUNCT
ap-8157	174	1	flight	flight	NOUN
ap-8157	174	2	velocity	velocity	NOUN
ap-8157	174	3	.	.	PUNCT
ap-8157	175	1	this	this	PRON
ap-8157	175	2	leads	lead	VERB
ap-8157	175	3	to	to	ADP
ap-8157	175	4	the	the	DET
ap-8157	175	5	necessity	necessity	NOUN
ap-8157	175	6	of	of	ADP
ap-8157	175	7	a	a	DET
ap-8157	175	8	tradeoff	tradeoff	NOUN
ap-8157	175	9	for	for	ADP
ap-8157	175	10	chosing	chose	VERB
ap-8157	175	11	the	the	DET
ap-8157	175	12	optimal	optimal	ADJ
ap-8157	175	13	system	system	NOUN
ap-8157	175	14	configuration	configuration	NOUN
ap-8157	175	15	.	.	PUNCT
ap-8157	176	1	the	the	DET
ap-8157	176	2	influence	influence	NOUN
ap-8157	176	3	of	of	ADP
ap-8157	176	4	various	various	ADJ
ap-8157	176	5	design	design	NOUN
ap-8157	176	6	parameters	parameter	NOUN
ap-8157	176	7	on	on	ADP
ap-8157	176	8	the	the	DET
ap-8157	176	9	propulsion	propulsion	NOUN
ap-8157	176	10	performance	performance	NOUN
ap-8157	176	11	is	be	AUX
ap-8157	176	12	presented	present	VERB
ap-8157	176	13	for	for	ADP
ap-8157	176	14	the	the	DET
ap-8157	176	15	expected	expect	VERB
ap-8157	176	16	range	range	NOUN
ap-8157	176	17	of	of	ADP
ap-8157	176	18	flight	flight	NOUN
ap-8157	176	19	velocities	velocity	NOUN
ap-8157	176	20	.	.	PUNCT
ap-8157	177	1	the	the	DET
ap-8157	177	2	proposed	propose	VERB
ap-8157	177	3	selection	selection	NOUN
ap-8157	177	4	of	of	ADP
ap-8157	177	5	the	the	DET
ap-8157	177	6	optimal	optimal	ADJ
ap-8157	177	7	variant	variant	NOUN
ap-8157	177	8	is	be	AUX
ap-8157	177	9	based	base	VERB
ap-8157	177	10	on	on	ADP
ap-8157	177	11	the	the	DET
ap-8157	177	12	maximum	maximum	NOUN
ap-8157	177	13	of	of	ADP
ap-8157	177	14	mean	mean	ADJ
ap-8157	177	15	relative	relative	ADJ
ap-8157	177	16	thrust	thrust	NOUN
ap-8157	177	17	for	for	ADP
ap-8157	177	18	the	the	DET
ap-8157	177	19	static	static	ADJ
ap-8157	177	20	case	case	NOUN
ap-8157	177	21	(	(	PUNCT
ap-8157	177	22	i.e.	i.e.	X
ap-8157	177	23	flight	flight	NOUN
ap-8157	177	24	velocity	velocity	NOUN
ap-8157	177	25	of	of	ADP
ap-8157	177	26	0	0	NUM
ap-8157	177	27	km	km	PROPN
ap-8157	177	28	h−1	h−1	PROPN
ap-8157	177	29	)	)	PUNCT
ap-8157	177	30	and	and	CCONJ
ap-8157	177	31	the	the	DET
ap-8157	177	32	expected	expect	VERB
ap-8157	177	33	high	high	ADJ
ap-8157	177	34	speed	speed	NOUN
ap-8157	177	35	cruise	cruise	NOUN
ap-8157	177	36	(	(	PUNCT
ap-8157	177	37	i.e.	i.e.	X
ap-8157	177	38	flight	flight	NOUN
ap-8157	177	39	velocity	velocity	NOUN
ap-8157	177	40	of	of	ADP
ap-8157	177	41	300	300	NUM
ap-8157	177	42	km	km	NOUN
ap-8157	177	43	h−1	h−1	PROPN
ap-8157	177	44	)	)	PUNCT
ap-8157	177	45	.	.	PUNCT
ap-8157	178	1	the	the	DET
ap-8157	178	2	presented	present	VERB
ap-8157	178	3	procedure	procedure	NOUN
ap-8157	178	4	and	and	CCONJ
ap-8157	178	5	the	the	DET
ap-8157	178	6	results	result	NOUN
ap-8157	178	7	can	can	AUX
ap-8157	178	8	be	be	AUX
ap-8157	178	9	used	use	VERB
ap-8157	178	10	for	for	ADP
ap-8157	178	11	a	a	DET
ap-8157	178	12	ducted	ducte	VERB
ap-8157	178	13	fan	fan	NOUN
ap-8157	178	14	design	design	NOUN
ap-8157	178	15	for	for	ADP
ap-8157	178	16	an	an	DET
ap-8157	178	17	electric	electric	ADJ
ap-8157	178	18	powered	power	VERB
ap-8157	178	19	aircraft	aircraft	NOUN
ap-8157	178	20	.	.	PUNCT
ap-8157	179	1	list	list	NOUN
ap-8157	179	2	of	of	ADP
ap-8157	179	3	symbols	symbol	NOUN
ap-8157	179	4	a	a	DET
ap-8157	179	5	speed	speed	NOUN
ap-8157	179	6	of	of	ADP
ap-8157	179	7	sound	sound	NOUN
ap-8157	179	8	[	[	X
ap-8157	179	9	m	m	NOUN
ap-8157	179	10	s−1	s−1	PROPN
ap-8157	179	11	]	]	PUNCT
ap-8157	179	12	a	a	DET
ap-8157	179	13	cross	cross	ADJ
ap-8157	179	14	-	-	ADJ
ap-8157	179	15	section	section	ADJ
ap-8157	179	16	area	area	NOUN
ap-8157	179	17	of	of	ADP
ap-8157	179	18	a	a	DET
ap-8157	179	19	duct	duct	NOUN
ap-8157	179	20	[	[	X
ap-8157	179	21	m2	m2	X
ap-8157	179	22	]	]	X
ap-8157	179	23	cp	cp	NUM
ap-8157	179	24	specific	specific	ADJ
ap-8157	179	25	heat	heat	NOUN
ap-8157	179	26	at	at	ADP
ap-8157	179	27	constant	constant	ADJ
ap-8157	179	28	pressure	pressure	NOUN
ap-8157	179	29	[	[	X
ap-8157	179	30	j	j	PROPN
ap-8157	179	31	kg−1	kg−1	PROPN
ap-8157	179	32	k−1	k−1	PROPN
ap-8157	179	33	]	]	PUNCT
ap-8157	179	34	d1	d1	PROPN
ap-8157	179	35	fan	fan	PROPN
ap-8157	179	36	diameter	diameter	NOUN
ap-8157	180	1	[	[	X
ap-8157	180	2	m	m	X
ap-8157	180	3	]	]	X
ap-8157	180	4	l	l	NOUN
ap-8157	180	5	duct	duct	NOUN
ap-8157	180	6	length	length	NOUN
ap-8157	180	7	[	[	X
ap-8157	180	8	m	m	X
ap-8157	180	9	]	]	X
ap-8157	180	10	555	555	NUM
ap-8157	180	11	jan	jan	PROPN
ap-8157	180	12	klesa	klesa	PROPN
ap-8157	180	13	acta	acta	PROPN
ap-8157	180	14	polytechnica	polytechnica	PROPN
ap-8157	180	15	figure	figure	NOUN
ap-8157	180	16	18	18	NUM
ap-8157	180	17	.	.	PUNCT
ap-8157	181	1	dependence	dependence	NOUN
ap-8157	181	2	of	of	ADP
ap-8157	181	3	relative	relative	ADJ
ap-8157	181	4	thrust	thrust	NOUN
ap-8157	181	5	on	on	ADP
ap-8157	181	6	nozzle	nozzle	NOUN
ap-8157	181	7	contraction	contraction	NOUN
ap-8157	181	8	ratio	ratio	NOUN
ap-8157	181	9	a1	a1	PROPN
ap-8157	181	10	/	/	SYM
ap-8157	181	11	a3	a3	NOUN
ap-8157	181	12	at	at	ADP
ap-8157	181	13	flight	flight	NOUN
ap-8157	181	14	speed	speed	NOUN
ap-8157	181	15	0	0	NUM
ap-8157	181	16	and	and	CCONJ
ap-8157	181	17	300	300	NUM
ap-8157	181	18	km	km	NOUN
ap-8157	181	19	h−1	h−1	PROPN
ap-8157	181	20	.	.	PUNCT
ap-8157	182	1	the	the	DET
ap-8157	182	2	selected	select	VERB
ap-8157	182	3	nozzle	nozzle	NOUN
ap-8157	182	4	contraction	contraction	NOUN
ap-8157	182	5	ratio	ratio	NOUN
ap-8157	182	6	a1	a1	PROPN
ap-8157	182	7	/	/	SYM
ap-8157	182	8	a3	a3	NOUN
ap-8157	182	9	=	=	SYM
ap-8157	182	10	1.17	1.17	NUM
ap-8157	182	11	is	be	AUX
ap-8157	182	12	marked	mark	VERB
ap-8157	182	13	by	by	ADP
ap-8157	182	14	dashed	dash	VERB
ap-8157	182	15	line	line	NOUN
ap-8157	182	16	.	.	PUNCT
ap-8157	183	1	figure	figure	NOUN
ap-8157	183	2	19	19	NUM
ap-8157	183	3	.	.	PUNCT
ap-8157	184	1	thrust	thrust	VERB
ap-8157	184	2	over	over	ADP
ap-8157	184	3	flight	flight	NOUN
ap-8157	184	4	speed	speed	NOUN
ap-8157	184	5	for	for	ADP
ap-8157	184	6	chosen	choose	VERB
ap-8157	184	7	fan	fan	NOUN
ap-8157	184	8	parameters	parameter	NOUN
ap-8157	184	9	,	,	PUNCT
ap-8157	184	10	i.e.	i.e.	X
ap-8157	184	11	d1	d1	NOUN
ap-8157	184	12	=	=	PROPN
ap-8157	184	13	0.66	0.66	NUM
ap-8157	184	14	m	m	NOUN
ap-8157	184	15	and	and	CCONJ
ap-8157	184	16	a1	a1	NOUN
ap-8157	184	17	/	/	SYM
ap-8157	184	18	a3	a3	NOUN
ap-8157	184	19	=	=	SYM
ap-8157	185	1	1.17	1.17	NUM
ap-8157	185	2	.	.	PUNCT
ap-8157	185	3	figure	figure	NOUN
ap-8157	185	4	20	20	NUM
ap-8157	185	5	.	.	PUNCT
ap-8157	186	1	propulsive	propulsive	ADJ
ap-8157	186	2	efficiency	efficiency	NOUN
ap-8157	186	3	over	over	ADP
ap-8157	186	4	flight	flight	NOUN
ap-8157	186	5	speed	speed	NOUN
ap-8157	186	6	for	for	ADP
ap-8157	186	7	chosen	choose	VERB
ap-8157	186	8	fan	fan	NOUN
ap-8157	186	9	parameters	parameter	NOUN
ap-8157	186	10	,	,	PUNCT
ap-8157	186	11	i.e.	i.e.	X
ap-8157	186	12	d1	d1	NOUN
ap-8157	186	13	=	=	PROPN
ap-8157	186	14	0.66	0.66	NUM
ap-8157	186	15	m	m	NOUN
ap-8157	186	16	and	and	CCONJ
ap-8157	186	17	a1	a1	NOUN
ap-8157	186	18	/	/	SYM
ap-8157	186	19	a3	a3	NOUN
ap-8157	186	20	=	=	SYM
ap-8157	186	21	1.17	1.17	NUM
ap-8157	186	22	.	.	PUNCT
ap-8157	186	23	figure	figure	NOUN
ap-8157	186	24	21	21	NUM
ap-8157	186	25	.	.	PUNCT
ap-8157	187	1	fan	fan	NOUN
ap-8157	187	2	pressure	pressure	NOUN
ap-8157	187	3	ratio	ratio	NOUN
ap-8157	187	4	over	over	ADP
ap-8157	187	5	flight	flight	NOUN
ap-8157	187	6	speed	speed	NOUN
ap-8157	187	7	for	for	ADP
ap-8157	187	8	chosen	choose	VERB
ap-8157	187	9	fan	fan	NOUN
ap-8157	187	10	parameters	parameter	NOUN
ap-8157	187	11	,	,	PUNCT
ap-8157	187	12	i.e.	i.e.	X
ap-8157	187	13	d1	d1	NOUN
ap-8157	187	14	=	=	PROPN
ap-8157	187	15	0.66	0.66	NUM
ap-8157	187	16	m	m	NOUN
ap-8157	187	17	and	and	CCONJ
ap-8157	187	18	a1	a1	NOUN
ap-8157	187	19	/	/	SYM
ap-8157	187	20	a3	a3	NOUN
ap-8157	187	21	=	=	SYM
ap-8157	188	1	1.17	1.17	NUM
ap-8157	188	2	.	.	PUNCT
ap-8157	189	1	figure	figure	NOUN
ap-8157	189	2	22	22	NUM
ap-8157	189	3	.	.	PUNCT
ap-8157	190	1	fan	fan	PROPN
ap-8157	190	2	axial	axial	ADJ
ap-8157	190	3	velocity	velocity	NOUN
ap-8157	190	4	component	component	NOUN
ap-8157	190	5	over	over	ADP
ap-8157	190	6	flight	flight	NOUN
ap-8157	190	7	speed	speed	NOUN
ap-8157	190	8	for	for	ADP
ap-8157	190	9	chosen	choose	VERB
ap-8157	190	10	fan	fan	NOUN
ap-8157	190	11	parameters	parameter	NOUN
ap-8157	190	12	,	,	PUNCT
ap-8157	190	13	i.e.	i.e.	X
ap-8157	190	14	d1	d1	NOUN
ap-8157	190	15	=	=	PROPN
ap-8157	190	16	0.66	0.66	NUM
ap-8157	190	17	m	m	NOUN
ap-8157	190	18	and	and	CCONJ
ap-8157	190	19	a1	a1	NOUN
ap-8157	190	20	/	/	SYM
ap-8157	190	21	a3	a3	NOUN
ap-8157	190	22	=	=	SYM
ap-8157	191	1	1.17	1.17	NUM
ap-8157	191	2	.	.	PUNCT
ap-8157	191	3	figure	figure	NOUN
ap-8157	191	4	23	23	NUM
ap-8157	191	5	.	.	PUNCT
ap-8157	192	1	fan	fan	PROPN
ap-8157	192	2	rpm	rpm	PROPN
ap-8157	192	3	over	over	ADP
ap-8157	192	4	flight	flight	NOUN
ap-8157	192	5	speed	speed	NOUN
ap-8157	192	6	for	for	ADP
ap-8157	192	7	chosen	choose	VERB
ap-8157	192	8	fan	fan	NOUN
ap-8157	192	9	parameters	parameter	NOUN
ap-8157	192	10	,	,	PUNCT
ap-8157	192	11	i.e.	i.e.	X
ap-8157	192	12	d1	d1	NOUN
ap-8157	192	13	=	=	PROPN
ap-8157	192	14	0.66	0.66	NUM
ap-8157	192	15	m	m	NOUN
ap-8157	192	16	and	and	CCONJ
ap-8157	192	17	a1	a1	NOUN
ap-8157	192	18	/	/	SYM
ap-8157	192	19	a3	a3	NOUN
ap-8157	192	20	=	=	PUNCT
ap-8157	192	21	1.17	1.17	NUM
ap-8157	192	22	.	.	PUNCT
ap-8157	193	1	556	556	NUM
ap-8157	193	2	vol	vol	NOUN
ap-8157	193	3	.	.	PUNCT
ap-8157	194	1	62	62	NUM
ap-8157	194	2	no	no	INTJ
ap-8157	194	3	.	.	PUNCT
ap-8157	195	1	5/2022	5/2022	NOUN
ap-8157	195	2	determination	determination	NOUN
ap-8157	195	3	of	of	ADP
ap-8157	195	4	fan	fan	NOUN
ap-8157	195	5	design	design	NOUN
ap-8157	195	6	parameters	parameter	NOUN
ap-8157	195	7	for	for	ADP
ap-8157	195	8	light	light	ADJ
ap-8157	195	9	-	-	PUNCT
ap-8157	195	10	sport	sport	NOUN
ap-8157	195	11	aircraft	aircraft	NOUN
ap-8157	195	12	ṁ	ṁ	PROPN
ap-8157	195	13	air	air	NOUN
ap-8157	195	14	mass	mass	PROPN
ap-8157	195	15	flow	flow	NOUN
ap-8157	195	16	[	[	X
ap-8157	195	17	kg	kg	X
ap-8157	195	18	s−1	s−1	PROPN
ap-8157	195	19	]	]	PUNCT
ap-8157	195	20	m	m	VERB
ap-8157	195	21	mach	mach	NOUN
ap-8157	195	22	number	number	NOUN
ap-8157	196	1	nm	nm	NOUN
ap-8157	196	2	fan	fan	NOUN
ap-8157	196	3	rpm	rpm	NOUN
ap-8157	196	4	[	[	X
ap-8157	196	5	rpm	rpm	X
ap-8157	196	6	]	]	X
ap-8157	196	7	ps	ps	NOUN
ap-8157	196	8	static	static	ADJ
ap-8157	196	9	pressure	pressure	NOUN
ap-8157	196	10	[	[	X
ap-8157	196	11	pa	pa	X
ap-8157	196	12	]	]	X
ap-8157	196	13	pt	pt	X
ap-8157	196	14	total	total	ADJ
ap-8157	196	15	pressure	pressure	NOUN
ap-8157	197	1	[	[	X
ap-8157	197	2	pa	pa	X
ap-8157	197	3	]	]	X
ap-8157	197	4	p	p	X
ap-8157	197	5	engine	engine	NOUN
ap-8157	197	6	power	power	NOUN
ap-8157	198	1	[	[	X
ap-8157	198	2	w	w	X
ap-8157	198	3	]	]	X
ap-8157	198	4	r	r	NOUN
ap-8157	198	5	air	air	NOUN
ap-8157	198	6	specific	specific	ADJ
ap-8157	198	7	gas	gas	NOUN
ap-8157	198	8	constant	constant	ADJ
ap-8157	198	9	[	[	X
ap-8157	198	10	j	j	X
ap-8157	198	11	kg−1	kg−1	PROPN
ap-8157	198	12	k−1	k−1	PROPN
ap-8157	198	13	]	]	PUNCT
ap-8157	198	14	t	t	PROPN
ap-8157	198	15	thrust	thrust	VERB
ap-8157	198	16	[	[	X
ap-8157	198	17	n	n	X
ap-8157	198	18	]	]	X
ap-8157	198	19	tt	tt	PROPN
ap-8157	198	20	total	total	ADJ
ap-8157	198	21	temperature	temperature	NOUN
ap-8157	199	1	[	[	X
ap-8157	199	2	k	k	X
ap-8157	199	3	]	]	X
ap-8157	199	4	ts	ts	ADP
ap-8157	199	5	static	static	ADJ
ap-8157	199	6	temperature	temperature	NOUN
ap-8157	200	1	[	[	X
ap-8157	200	2	k	k	X
ap-8157	200	3	]	]	X
ap-8157	200	4	v	v	ADP
ap-8157	200	5	velocity	velocity	NOUN
ap-8157	200	6	[	[	X
ap-8157	200	7	m	m	NOUN
ap-8157	200	8	s−1	s−1	PROPN
ap-8157	200	9	]	]	PUNCT
ap-8157	200	10	η	η	PROPN
ap-8157	200	11	efficiency	efficiency	NOUN
ap-8157	200	12	ζ	ζ	NOUN
ap-8157	200	13	pressure	pressure	NOUN
ap-8157	200	14	loss	loss	NOUN
ap-8157	200	15	coefficient	coefficient	NOUN
ap-8157	200	16	κ	κ	ADP
ap-8157	200	17	ratio	ratio	NOUN
ap-8157	200	18	of	of	ADP
ap-8157	200	19	specific	specific	ADJ
ap-8157	200	20	heats	heat	NOUN
ap-8157	200	21	λ	λ	PROPN
ap-8157	200	22	wall	wall	NOUN
ap-8157	200	23	friction	friction	NOUN
ap-8157	200	24	factor	factor	NOUN
ap-8157	200	25	π12	π12	VERB
ap-8157	200	26	fan	fan	NOUN
ap-8157	200	27	pressure	pressure	NOUN
ap-8157	200	28	ratio	ratio	NOUN
ap-8157	200	29	ρ	ρ	PROPN
ap-8157	200	30	air	air	NOUN
ap-8157	200	31	density	density	NOUN
ap-8157	201	1	[	[	X
ap-8157	201	2	kg	kg	X
ap-8157	201	3	m−3	m−3	PROPN
ap-8157	201	4	]	]	X
ap-8157	201	5	(	(	PUNCT
ap-8157	201	6	ρv	ρv	NOUN
ap-8157	201	7	)	)	PUNCT
ap-8157	201	8	flow	flow	NOUN
ap-8157	201	9	density	density	NOUN
ap-8157	202	1	[	[	X
ap-8157	202	2	kg	kg	X
ap-8157	202	3	m−2	m−2	PROPN
ap-8157	202	4	s−1	s−1	PROPN
ap-8157	202	5	]	]	PUNCT
ap-8157	202	6	(	(	PUNCT
ap-8157	202	7	ρv)c	ρv)c	NUM
ap-8157	202	8	critical	critical	ADJ
ap-8157	202	9	flow	flow	NOUN
ap-8157	202	10	density	density	NOUN
ap-8157	203	1	[	[	X
ap-8157	203	2	kg	kg	X
ap-8157	203	3	m−2	m−2	PROPN
ap-8157	203	4	s−1	s−1	PROPN
ap-8157	203	5	]	]	PUNCT
ap-8157	203	6	acknowledgements	acknowledgement	NOUN
ap-8157	203	7	this	this	DET
ap-8157	203	8	work	work	NOUN
ap-8157	203	9	was	be	AUX
ap-8157	203	10	supported	support	VERB
ap-8157	203	11	by	by	ADP
ap-8157	203	12	technology	technology	NOUN
ap-8157	203	13	agency	agency	NOUN
ap-8157	203	14	of	of	ADP
ap-8157	203	15	the	the	DET
ap-8157	203	16	czech	czech	PROPN
ap-8157	203	17	republic	republic	NOUN
ap-8157	203	18	,	,	PUNCT
ap-8157	203	19	grant	grant	VERB
ap-8157	203	20	no	no	INTJ
ap-8157	204	1	.	.	PUNCT
ap-8157	204	2	fv40263	fv40263	PROPN
ap-8157	204	3	.	.	PUNCT
ap-8157	205	1	references	reference	NOUN
ap-8157	205	2	[	[	X
ap-8157	205	3	1	1	NUM
ap-8157	205	4	]	]	PUNCT
ap-8157	205	5	m.	m.	NOUN
ap-8157	205	6	hepperle	hepperle	PROPN
ap-8157	205	7	.	.	PUNCT
ap-8157	206	1	electric	electric	ADJ
ap-8157	206	2	flight	flight	NOUN
ap-8157	206	3	–	–	PUNCT
ap-8157	206	4	potential	potential	NOUN
ap-8157	206	5	and	and	CCONJ
ap-8157	206	6	limitations	limitation	NOUN
ap-8157	206	7	.	.	PUNCT
ap-8157	207	1	energy	energy	NOUN
ap-8157	207	2	efficient	efficient	ADJ
ap-8157	207	3	technologies	technology	NOUN
ap-8157	207	4	and	and	CCONJ
ap-8157	207	5	concepts	concept	NOUN
ap-8157	207	6	of	of	ADP
ap-8157	207	7	operation	operation	NOUN
ap-8157	207	8	(	(	PUNCT
ap-8157	207	9	sto	sto	PROPN
ap-8157	207	10	-	-	PUNCT
ap-8157	207	11	mp	mp	NOUN
ap-8157	207	12	-	-	PUNCT
ap-8157	207	13	avt-209	avt-209	NOUN
ap-8157	207	14	)	)	PUNCT
ap-8157	207	15	,	,	PUNCT
ap-8157	207	16	2012	2012	NUM
ap-8157	207	17	.	.	PUNCT
ap-8157	208	1	accessed	access	VERB
ap-8157	208	2	2022	2022	NUM
ap-8157	208	3	-	-	SYM
ap-8157	208	4	10	10	NUM
ap-8157	208	5	-	-	SYM
ap-8157	208	6	26	26	NUM
ap-8157	208	7	,	,	PUNCT
ap-8157	208	8	https://elib.dlr.de/78726/.	https://elib.dlr.de/78726/.	PUNCT
ap-8157	209	1	[	[	X
ap-8157	209	2	2	2	NUM
ap-8157	209	3	]	]	X
ap-8157	209	4	electric	electric	PROPN
ap-8157	209	5	&	&	CCONJ
ap-8157	209	6	hybrid	hybrid	ADJ
ap-8157	209	7	-	-	PUNCT
ap-8157	209	8	electric	electric	ADJ
ap-8157	209	9	propulsion	propulsion	NOUN
ap-8157	209	10	,	,	PUNCT
ap-8157	209	11	2022	2022	NUM
ap-8157	209	12	.	.	PUNCT
ap-8157	209	13	accessed	access	VERB
ap-8157	209	14	2022	2022	NUM
ap-8157	209	15	-	-	SYM
ap-8157	209	16	10	10	NUM
ap-8157	209	17	-	-	SYM
ap-8157	209	18	26	26	NUM
ap-8157	209	19	,	,	PUNCT
ap-8157	209	20	https	https	NOUN
ap-8157	209	21	:	:	PUNCT
ap-8157	209	22	//aerospace.honeywell.com	//aerospace.honeywell.com	SYM
ap-8157	209	23	/	/	SYM
ap-8157	209	24	us	we	PRON
ap-8157	209	25	/	/	SYM
ap-8157	209	26	en	en	NOUN
ap-8157	209	27	/	/	SYM
ap-8157	209	28	products	product	NOUN
ap-8157	209	29	-	-	PUNCT
ap-8157	209	30	andservices	andservice	NOUN
ap-8157	209	31	/	/	SYM
ap-8157	209	32	product	product	NOUN
ap-8157	209	33	/	/	SYM
ap-8157	209	34	hardware	hardware	NOUN
ap-8157	209	35	-	-	PUNCT
ap-8157	209	36	and	and	CCONJ
ap-8157	209	37	-	-	PUNCT
ap-8157	209	38	systems	system	NOUN
ap-8157	209	39	/	/	SYM
ap-8157	209	40	electricpower	electricpower	NOUN
ap-8157	209	41	/	/	SYM
ap-8157	209	42	hybrid	hybrid	NOUN
ap-8157	209	43	-	-	PUNCT
ap-8157	209	44	electric	electric	ADJ
ap-8157	209	45	-	-	PUNCT
ap-8157	209	46	electric	electric	ADJ
ap-8157	209	47	-	-	PUNCT
ap-8157	209	48	propulsion	propulsion	NOUN
ap-8157	209	49	.	.	PUNCT
ap-8157	210	1	[	[	X
ap-8157	210	2	3	3	NUM
ap-8157	210	3	]	]	ADJ
ap-8157	210	4	rolls	rolls	PROPN
ap-8157	210	5	-	-	PUNCT
ap-8157	210	6	royce	royce	PROPN
ap-8157	210	7	plc	plc	PROPN
ap-8157	210	8	.	.	PUNCT
ap-8157	210	9	rolls	rolls	PROPN
ap-8157	210	10	-	-	PUNCT
ap-8157	210	11	royce	royce	PROPN
ap-8157	210	12	advances	advance	VERB
ap-8157	210	13	hybrid	hybrid	NOUN
ap-8157	210	14	-	-	PUNCT
ap-8157	210	15	electric	electric	ADJ
ap-8157	210	16	flight	flight	NOUN
ap-8157	210	17	with	with	ADP
ap-8157	210	18	new	new	ADJ
ap-8157	210	19	technology	technology	NOUN
ap-8157	210	20	to	to	PART
ap-8157	210	21	lead	lead	VERB
ap-8157	210	22	the	the	DET
ap-8157	210	23	way	way	NOUN
ap-8157	210	24	in	in	ADP
ap-8157	210	25	advanced	advanced	ADJ
ap-8157	210	26	air	air	NOUN
ap-8157	210	27	mobility	mobility	NOUN
ap-8157	210	28	,	,	PUNCT
ap-8157	210	29	2022	2022	NUM
ap-8157	210	30	.	.	PUNCT
ap-8157	211	1	accessed	access	VERB
ap-8157	211	2	2022	2022	NUM
ap-8157	211	3	-	-	SYM
ap-8157	211	4	10	10	NUM
ap-8157	211	5	-	-	SYM
ap-8157	211	6	26	26	NUM
ap-8157	211	7	,	,	PUNCT
ap-8157	211	8	https://www.rolls-royce.com/media/pressreleases/2022/22-06-2022-rr-advances-hybridelectric-flight-with-new-technology.aspx	https://www.rolls-royce.com/media/pressreleases/2022/22-06-2022-rr-advances-hybridelectric-flight-with-new-technology.aspx	NOUN
ap-8157	211	9	.	.	PUNCT
ap-8157	212	1	[	[	X
ap-8157	212	2	4	4	X
ap-8157	212	3	]	]	PUNCT
ap-8157	212	4	s.	s.	PROPN
ap-8157	212	5	d.	d.	PROPN
ap-8157	212	6	v.	v.	PROPN
ap-8157	212	7	weelden	weelden	PROPN
ap-8157	212	8	,	,	PUNCT
ap-8157	212	9	d.	d.	PROPN
ap-8157	212	10	e.	e.	PROPN
ap-8157	212	11	smith	smith	PROPN
ap-8157	212	12	,	,	PUNCT
ap-8157	212	13	b.	b.	PROPN
ap-8157	212	14	r.	r.	PROPN
ap-8157	212	15	mullins	mullins	PROPN
ap-8157	212	16	.	.	PROPN
ap-8157	212	17	preliminary	preliminary	ADJ
ap-8157	212	18	design	design	NOUN
ap-8157	212	19	of	of	ADP
ap-8157	212	20	a	a	DET
ap-8157	212	21	ducted	ducte	VERB
ap-8157	212	22	fan	fan	NOUN
ap-8157	212	23	propulsion	propulsion	NOUN
ap-8157	212	24	system	system	NOUN
ap-8157	212	25	for	for	ADP
ap-8157	212	26	general	general	ADJ
ap-8157	212	27	aviation	aviation	NOUN
ap-8157	212	28	aircraft	aircraft	NOUN
ap-8157	212	29	.	.	PUNCT
ap-8157	213	1	in	in	ADP
ap-8157	213	2	aiaa	aiaa	PROPN
ap-8157	213	3	34th	34th	ADJ
ap-8157	213	4	aerospace	aerospace	NOUN
ap-8157	213	5	sciences	sciences	PROPN
ap-8157	213	6	meeting	meeting	NOUN
ap-8157	213	7	and	and	CCONJ
ap-8157	213	8	exibit	exibit	NOUN
ap-8157	213	9	,	,	PUNCT
ap-8157	213	10	96	96	NUM
ap-8157	213	11	-	-	SYM
ap-8157	213	12	0376	0376	NUM
ap-8157	213	13	.	.	PUNCT
ap-8157	214	1	https://doi.org/10.2514/6.1996-376	https://doi.org/10.2514/6.1996-376	PROPN
ap-8157	214	2	.	.	PUNCT
ap-8157	215	1	[	[	X
ap-8157	215	2	5	5	NUM
ap-8157	215	3	]	]	X
ap-8157	215	4	letecká	letecká	NOUN
ap-8157	215	5	amatérská	amatérská	ADJ
ap-8157	215	6	asociace	asociace	NOUN
ap-8157	215	7	čr	čr	PROPN
ap-8157	215	8	.	.	PUNCT
ap-8157	216	1	ul	ul	PROPN
ap-8157	216	2	2	2	NUM
ap-8157	216	3	část	část	PROPN
ap-8157	216	4	i.	i.	NOUN
ap-8157	216	5	,	,	PUNCT
ap-8157	216	6	2019	2019	NUM
ap-8157	216	7	.	.	PUNCT
ap-8157	217	1	accessed	access	VERB
ap-8157	217	2	2022	2022	NUM
ap-8157	217	3	-	-	SYM
ap-8157	217	4	10	10	NUM
ap-8157	217	5	-	-	SYM
ap-8157	217	6	26	26	NUM
ap-8157	217	7	,	,	PUNCT
ap-8157	217	8	https://www.laacr.cz/	https://www.laacr.cz/	NUM
ap-8157	217	9	sitecollectiondocuments	sitecollectiondocument	NOUN
ap-8157	217	10	/	/	SYM
ap-8157	217	11	predpisy	predpisy	ADJ
ap-8157	217	12	/	/	SYM
ap-8157	217	13	ul2%20%c4%8d%	ul2%20%c4%8d%	ADJ
ap-8157	217	14	c3%a1st%20i_26.3.2019.pdf	c3%a1st%20i_26.3.2019.pdf	NOUN
ap-8157	217	15	.	.	PUNCT
ap-8157	218	1	[	[	X
ap-8157	218	2	6	6	NUM
ap-8157	218	3	]	]	X
ap-8157	218	4	deutscher	deutscher	PROPN
ap-8157	218	5	aero	aero	PROPN
ap-8157	218	6	club	club	PROPN
ap-8157	218	7	.	.	PUNCT
ap-8157	219	1	lufttüchtigkeitsforderungen	lufttüchtigkeitsforderungen	PROPN
ap-8157	219	2	für	für	PROPN
ap-8157	219	3	aerodynamisch	aerodynamisch	VERB
ap-8157	219	4	gesteuerte	gesteuerte	PROPN
ap-8157	219	5	ultraleichtflugzeuge	ultraleichtflugzeuge	ADJ
ap-8157	219	6	ltf	ltf	PROPN
ap-8157	219	7	-	-	PUNCT
ap-8157	219	8	ul	ul	PROPN
ap-8157	219	9	vom	vom	NOUN
ap-8157	219	10	15.01.2019	15.01.2019	NUM
ap-8157	219	11	und	und	NOUN
ap-8157	219	12	änderung	änderung	PROPN
ap-8157	219	13	vom	vom	PROPN
ap-8157	219	14	28.02.2019	28.02.2019	NUM
ap-8157	219	15	(	(	PUNCT
ap-8157	219	16	nfl	nfl	PROPN
ap-8157	219	17	2	2	NUM
ap-8157	219	18	-	-	SYM
ap-8157	219	19	459	459	NUM
ap-8157	219	20	-	-	SYM
ap-8157	219	21	19	19	NUM
ap-8157	219	22	)	)	PUNCT
ap-8157	219	23	,	,	PUNCT
ap-8157	219	24	2019	2019	NUM
ap-8157	219	25	.	.	PUNCT
ap-8157	220	1	accessed	access	VERB
ap-8157	220	2	2022	2022	NUM
ap-8157	220	3	-	-	SYM
ap-8157	220	4	10	10	NUM
ap-8157	220	5	-	-	SYM
ap-8157	220	6	26	26	NUM
ap-8157	220	7	,	,	PUNCT
ap-8157	220	8	https	https	NOUN
ap-8157	220	9	:	:	PUNCT
ap-8157	220	10	//www.daec.de	//www.daec.de	ADJ
ap-8157	220	11	/	/	SYM
ap-8157	220	12	fileadmin	fileadmin	ADJ
ap-8157	220	13	/	/	SYM
ap-8157	220	14	user_upload	user_upload	ADJ
ap-8157	220	15	/	/	SYM
ap-8157	220	16	files/2019/	files/2019/	PROPN
ap-8157	220	17	luftsportgeraete_buero	luftsportgeraete_buero	PROPN
ap-8157	220	18	/	/	SYM
ap-8157	220	19	ltf	ltf	PROPN
ap-8157	220	20	/	/	SYM
ap-8157	220	21	ltf	ltf	PROPN
ap-8157	220	22	-	-	PUNCT
ap-8157	220	23	ul_2019.pdf	ul_2019.pdf	NOUN
ap-8157	220	24	.	.	PUNCT
ap-8157	221	1	[	[	X
ap-8157	221	2	7	7	X
ap-8157	221	3	]	]	X
ap-8157	221	4	n.	n.	ADJ
ap-8157	221	5	a.	a.	NOUN
ap-8157	221	6	cumpsty	cumpsty	NOUN
ap-8157	221	7	.	.	PUNCT
ap-8157	222	1	compressor	compressor	NOUN
ap-8157	222	2	aerodynamics	aerodynamic	NOUN
ap-8157	222	3	.	.	PUNCT
ap-8157	223	1	krieger	krieger	PROPN
ap-8157	223	2	publishing	publishing	PROPN
ap-8157	223	3	company	company	NOUN
ap-8157	223	4	,	,	PUNCT
ap-8157	223	5	2nd	2nd	ADJ
ap-8157	223	6	edn	edn	PROPN
ap-8157	223	7	.	.	PUNCT
ap-8157	223	8	,	,	PUNCT
ap-8157	223	9	2004	2004	NUM
ap-8157	223	10	.	.	PUNCT
ap-8157	224	1	[	[	X
ap-8157	224	2	8	8	NUM
ap-8157	224	3	]	]	X
ap-8157	224	4	r.	r.	PROPN
ap-8157	224	5	o.	o.	PROPN
ap-8157	224	6	bullock	bullock	PROPN
ap-8157	224	7	,	,	PUNCT
ap-8157	224	8	i.	i.	PROPN
ap-8157	224	9	a.	a.	PROPN
ap-8157	224	10	johnsen	johnsen	PROPN
ap-8157	224	11	.	.	PUNCT
ap-8157	225	1	aerodynamic	aerodynamic	ADJ
ap-8157	225	2	design	design	NOUN
ap-8157	225	3	of	of	ADP
ap-8157	225	4	axial	axial	ADJ
ap-8157	225	5	flow	flow	NOUN
ap-8157	225	6	compressors	compressor	NOUN
ap-8157	225	7	.	.	PUNCT
ap-8157	226	1	nasa	nasa	PROPN
ap-8157	226	2	-	-	PUNCT
ap-8157	226	3	sp-36	sp-36	NOUN
ap-8157	226	4	.	.	PUNCT
ap-8157	227	1	nasa	nasa	PROPN
ap-8157	227	2	lewis	lewis	PROPN
ap-8157	227	3	research	research	PROPN
ap-8157	227	4	center	center	PROPN
ap-8157	227	5	,	,	PUNCT
ap-8157	227	6	cleveland	cleveland	PROPN
ap-8157	227	7	,	,	PUNCT
ap-8157	227	8	oh	oh	INTJ
ap-8157	227	9	,	,	PUNCT
ap-8157	227	10	1965	1965	NUM
ap-8157	227	11	.	.	PUNCT
ap-8157	228	1	[	[	X
ap-8157	228	2	9	9	NUM
ap-8157	228	3	]	]	X
ap-8157	228	4	r.	r.	PROPN
ap-8157	228	5	theiner	theiner	PROPN
ap-8157	228	6	,	,	PUNCT
ap-8157	228	7	j.	j.	PROPN
ap-8157	228	8	brabec	brabec	PROPN
ap-8157	228	9	.	.	PUNCT
ap-8157	229	1	experience	experience	NOUN
ap-8157	229	2	with	with	ADP
ap-8157	229	3	the	the	DET
ap-8157	229	4	design	design	NOUN
ap-8157	229	5	of	of	ADP
ap-8157	229	6	ultralight	ultralight	ADJ
ap-8157	229	7	airplane	airplane	NOUN
ap-8157	229	8	with	with	ADP
ap-8157	229	9	unconventional	unconventional	ADJ
ap-8157	229	10	powerplant	powerplant	NOUN
ap-8157	229	11	.	.	PUNCT
ap-8157	230	1	proceedings	proceeding	NOUN
ap-8157	230	2	of	of	ADP
ap-8157	230	3	the	the	DET
ap-8157	230	4	institution	institution	NOUN
ap-8157	230	5	of	of	ADP
ap-8157	230	6	mechanical	mechanical	ADJ
ap-8157	230	7	engineers	engineer	NOUN
ap-8157	230	8	,	,	PUNCT
ap-8157	230	9	part	part	NOUN
ap-8157	230	10	g	g	NOUN
ap-8157	230	11	;	;	PUNCT
ap-8157	230	12	journal	journal	NOUN
ap-8157	230	13	of	of	ADP
ap-8157	230	14	aerospace	aerospace	NOUN
ap-8157	230	15	engineering	engineering	NOUN
ap-8157	230	16	232(14):2721–2733	232(14):2721–2733	NUM
ap-8157	230	17	,	,	PUNCT
ap-8157	230	18	2018	2018	NUM
ap-8157	230	19	.	.	PUNCT
ap-8157	231	1	https://doi.org/10.1177/0954410018774117	https://doi.org/10.1177/0954410018774117	PROPN
ap-8157	231	2	.	.	PUNCT
ap-8157	232	1	[	[	X
ap-8157	232	2	10	10	NUM
ap-8157	232	3	]	]	X
ap-8157	232	4	j.	j.	PROPN
ap-8157	232	5	hejna	hejna	PROPN
ap-8157	232	6	.	.	PUNCT
ap-8157	233	1	intake	intake	NOUN
ap-8157	233	2	desing	dese	VERB
ap-8157	233	3	for	for	ADP
ap-8157	233	4	experimental	experimental	ADJ
ap-8157	233	5	fan	fan	PROPN
ap-8157	233	6	.	.	PUNCT
ap-8157	234	1	master	master	PROPN
ap-8157	234	2	’s	’s	PART
ap-8157	234	3	thesis	thesis	NOUN
ap-8157	234	4	,	,	PUNCT
ap-8157	234	5	czech	czech	PROPN
ap-8157	234	6	technical	technical	PROPN
ap-8157	234	7	university	university	PROPN
ap-8157	234	8	in	in	ADP
ap-8157	234	9	prague	prague	PROPN
ap-8157	234	10	,	,	PUNCT
ap-8157	234	11	2021	2021	NUM
ap-8157	234	12	.	.	PUNCT
ap-8157	234	13	accessed	access	VERB
ap-8157	234	14	2022	2022	NUM
ap-8157	234	15	-	-	SYM
ap-8157	234	16	10	10	NUM
ap-8157	234	17	-	-	SYM
ap-8157	234	18	26	26	NUM
ap-8157	234	19	,	,	PUNCT
ap-8157	234	20	http://hdl.handle.net/10467/96889	http://hdl.handle.net/10467/96889	ADJ
ap-8157	234	21	.	.	PUNCT
ap-8157	235	1	[	[	X
ap-8157	235	2	11	11	NUM
ap-8157	235	3	]	]	PUNCT
ap-8157	235	4	s.	s.	PROPN
ap-8157	235	5	farokhi	farokhi	PROPN
ap-8157	235	6	.	.	PUNCT
ap-8157	235	7	aircraft	aircraft	NOUN
ap-8157	235	8	propulsion	propulsion	NOUN
ap-8157	235	9	.	.	PUNCT
ap-8157	236	1	john	john	PROPN
ap-8157	236	2	wiley	wiley	PROPN
ap-8157	236	3	&	&	CCONJ
ap-8157	236	4	sons	son	NOUN
ap-8157	236	5	,	,	PUNCT
ap-8157	236	6	2nd	2nd	ADJ
ap-8157	236	7	edn	edn	NOUN
ap-8157	236	8	.	.	PUNCT
ap-8157	236	9	,	,	PUNCT
ap-8157	236	10	2014	2014	NUM
ap-8157	236	11	.	.	PUNCT
ap-8157	237	1	[	[	X
ap-8157	237	2	12	12	NUM
ap-8157	237	3	]	]	PUNCT
ap-8157	237	4	s.	s.	PROPN
ap-8157	237	5	albrig	albrig	PROPN
ap-8157	237	6	.	.	PUNCT
ap-8157	238	1	angewandte	angewandte	PROPN
ap-8157	238	2	strömungslehre	strömungslehre	PROPN
ap-8157	238	3	.	.	PUNCT
ap-8157	239	1	akademie	akademie	PROPN
ap-8157	239	2	-	-	PUNCT
ap-8157	239	3	verlag	verlag	PROPN
ap-8157	239	4	,	,	PUNCT
ap-8157	239	5	5th	5th	ADJ
ap-8157	239	6	edn	edn	NOUN
ap-8157	239	7	.	.	PUNCT
ap-8157	239	8	,	,	PUNCT
ap-8157	239	9	1978	1978	NUM
ap-8157	239	10	.	.	PUNCT
ap-8157	240	1	557	557	NUM
ap-8157	240	2	https://elib.dlr.de/78726/	https://elib.dlr.de/78726/	PROPN
ap-8157	240	3	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	NOUN
ap-8157	240	4	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	NOUN
ap-8157	240	5	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	NOUN
ap-8157	240	6	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	https://aerospace.honeywell.com/us/en/products-and-services/product/hardware-and-systems/electric-power/hybrid-electric-electric-propulsion	NOUN
ap-8157	240	7	https://www.rolls-royce.com/media/press-releases/2022/22-06-2022-rr-advances-hybrid-electric-flight-with-new-technology.aspx	https://www.rolls-royce.com/media/press-releases/2022/22-06-2022-rr-advances-hybrid-electric-flight-with-new-technology.aspx	NOUN
ap-8157	240	8	https://www.rolls-royce.com/media/press-releases/2022/22-06-2022-rr-advances-hybrid-electric-flight-with-new-technology.aspx	https://www.rolls-royce.com/media/press-releases/2022/22-06-2022-rr-advances-hybrid-electric-flight-with-new-technology.aspx	NOUN
ap-8157	240	9	https://www.rolls-royce.com/media/press-releases/2022/22-06-2022-rr-advances-hybrid-electric-flight-with-new-technology.aspx	https://www.rolls-royce.com/media/press-releases/2022/22-06-2022-rr-advances-hybrid-electric-flight-with-new-technology.aspx	NOUN
ap-8157	240	10	https://doi.org/10.2514/6.1996-376	https://doi.org/10.2514/6.1996-376	PROPN
ap-8157	240	11	https://www.laacr.cz/sitecollectiondocuments/predpisy/ul2%20%c4%8d%c3%a1st%20i_26.3.2019.pdf	https://www.laacr.cz/sitecollectiondocuments/predpisy/ul2%20%c4%8d%c3%a1st%20i_26.3.2019.pdf	NOUN
ap-8157	240	12	https://www.laacr.cz/sitecollectiondocuments/predpisy/ul2%20%c4%8d%c3%a1st%20i_26.3.2019.pdf	https://www.laacr.cz/sitecollectiondocuments/predpisy/ul2%20%c4%8d%c3%a1st%20i_26.3.2019.pdf	PROPN
ap-8157	240	13	https://www.laacr.cz/sitecollectiondocuments/predpisy/ul2%20%c4%8d%c3%a1st%20i_26.3.2019.pdf	https://www.laacr.cz/sitecollectiondocuments/predpisy/ul2%20%c4%8d%c3%a1st%20i_26.3.2019.pdf	PROPN
ap-8157	240	14	https://www.daec.de/fileadmin/user_upload/files/2019/luftsportgeraete_buero/ltf/ltf-ul_2019.pdf	https://www.daec.de/fileadmin/user_upload/files/2019/luftsportgeraete_buero/ltf/ltf-ul_2019.pdf	PROPN
ap-8157	240	15	https://www.daec.de/fileadmin/user_upload/files/2019/luftsportgeraete_buero/ltf/ltf-ul_2019.pdf	https://www.daec.de/fileadmin/user_upload/files/2019/luftsportgeraete_buero/ltf/ltf-ul_2019.pdf	PROPN
ap-8157	240	16	https://www.daec.de/fileadmin/user_upload/files/2019/luftsportgeraete_buero/ltf/ltf-ul_2019.pdf	https://www.daec.de/fileadmin/user_upload/files/2019/luftsportgeraete_buero/ltf/ltf-ul_2019.pdf	PROPN
ap-8157	240	17	https://doi.org/10.1177/0954410018774117	https://doi.org/10.1177/0954410018774117	PROPN
ap-8157	240	18	http://hdl.handle.net/10467/96889	http://hdl.handle.net/10467/96889	PROPN
ap-8157	240	19	acta	acta	PROPN
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ap-8157	240	23	2022	2022	NUM
ap-8157	240	24	1	1	NUM
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ap-8157	240	26	2	2	NUM
ap-8157	240	27	methods	method	NOUN
ap-8157	240	28	2.1	2.1	NUM
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ap-8157	240	31	3	3	NUM
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ap-8157	240	33	4	4	NUM
ap-8157	240	34	discussion	discussion	NOUN
ap-8157	240	35	5	5	NUM
ap-8157	240	36	conclusions	conclusion	NOUN
ap-8157	240	37	list	list	NOUN
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ap-8157	240	39	symbols	symbol	NOUN
ap-8157	240	40	acknowledgements	acknowledgement	NOUN
ap-8157	240	41	references	reference	NOUN