id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
6q182j65s7w	Aaron J. Pope	Performance of a Subsonic Compressor Airfoil with Upstream, End-Wall Injection Flow	2020		.txt	text/plain	225	9	49	The exit of the cascade was interrogated by a five-hole-probe and a total pressure Kiel probe to provide total pressure measurements, which were used to calculate total pressure loss coefficients at the exit of the test section. The independent variables studied were airfoil incidence angle and mass flow rate of end-wall injection upstream of the stator.	cache/6q182j65s7w.txt	txt/6q182j65s7w.txt