id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
ap-556	Chudý, P.	Response of a Light Aircraft Under Gust Loads	2004	6	.pdf	application/pdf	2938	174	64	For single Input/Output systems, the PSD function of the response quantity, �(�), is related to the PSD function of the source, �(�), by � � � �( ) ( ) ( )� H i 2 � (2) where H i( )� is the frequency response function. 6: Power spectral density of T at the wing root Type of response A (N�m) N0 (Hz) M1 0.502 20.23 M2 8.263 3.105 T 0.389 20.12 Table 3: Summary of the probability parameters at the wing root station Altitude 1000.0 m True Air Speed 44.0 m�s�1 Dynamic pressure 1076.06 Pa Mach number 0.1308 Gust Velocity, U0 15.0 m�s�1 Table 4: Flight conditions for discrete gust analysis These points were placed at the CG and at the wing root.	cache/ap-556.pdf	txt/ap-556.txt