id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
ispiv-93	Aiura, Akira; Kobayashi, Kentaro; Sakakibara, Jun	Separation Control of NACA0015 Airfoil using Plasma Actuators	2021	2	.pdf	application/pdf	752	38	64	Surface pressure was monitored by pressure transducers through pressure taps on the upper surface of airfoil. However, such a predominance of the PA-off case is not maintained towards leading edge, i.e. the negative pressure value under the φ = π case exceeds others in a range from x = -0.1c to -0.2c, as indicated by PIV based pressure.	cache/ispiv-93.pdf	txt/ispiv-93.txt