id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
cf95j96242f	David M Schatzman	A Study of Unsteady Turbulent Boundary Layer Separation Under Conditions Relevant to Helicopter Rotor Dynamics	2011		.txt	text/plain	253	10	33	The implications of the experimental results for the development of flow control strategies for unsteady boundary layer separation are discussed. Downstream of the flat plate, a convex ramp section imposes a streamwise adverse pressure gradient that gives rise to boundary layer separation.	cache/cf95j96242f.txt	txt/cf95j96242f.txt