id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
hij-34	Ha, Kwangtae	Innovative Blade Trailing Edge Flap Design Concept using Flexible Torsion Bar and Worm Drive	2020	6	.pdf	application/pdf	2369	134	57	Schematic diagram of application to flexible trailing edge flap system on rotor blade The equilibrium equation of the flap device at hinge location O shown in in Figure 6 becomes 𝑇 + 𝑀𝑎𝑒𝑟𝑜(𝛼, 𝜃, 𝛺) = Xh: Distance of center of starbeam from aerodynamic center; Figure 6. (a) Aerodynamic force distribution; (a) and (b) deformed cross-sectional shape of flexible trailing edge flap system 5.	cache/hij-34.pdf	txt/hij-34.txt