id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
5q47rn31z85	Christopher L. Kelley	Airfoil Leading and Trailing Edge Separation Control Using SDBD Plasma Actuators	2013		.txt	text/plain	525	21	41	The NASA energy efficient transport (EET) airfoil was a platform to study the effect of plasma actuators on leading edge stall and boundary layer separation in a strong adverse pressure gradient, while the V-22 Osprey airfoil was used to study trailing edge stall with separation in a weaker adverse pressure gradient. The second part of the experiment examined the efficacy of plasma actuators on a V-22 airfoil for trailing edge separation control in the presence of new factors such as moving separation location, crossflow, turbulent boundary layers, and weaker pressure gradients at the line of vanishing shear.	cache/5q47rn31z85.txt	txt/5q47rn31z85.txt