id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
ap-4085	Schoř, Pavel	AERODYNAMIC LOAD OF AN AIRCRAFT WITH A HIGHLY ELASTIC WING	2017	10	.pdf	application/pdf	5164	338	64	Keywords: aerodynamics, panel method, finite element method, wing load, fluid structure interaction. Eligibility Based on assumptions made in Sections 2.1 and 2.2, the method presented in this article is suitable for analysis of quasi-static maneuvers of an aircraft with elastic wings, operating at a low Mach number (M < 0.3) and sufficiently high Reynolds number (Re > 1000000).	cache/ap-4085.pdf	txt/ap-4085.txt