id	author	title	date	pages	extension	mime	words	sentence	flesch	summary	cache	txt
02870v8624p	Nozomu Kato	Flow Phenomena under a Backpressure in an Axisymmetric Scramjet Model	2019		.txt	text/plain	590	27	55	The wall pressure measurement showed that there were pressure gradients in the isolator imposed by the incident shock wave for α = 6 and 9, whereas minor pressure gradients were present for α = 0. Three angled-wedge inlets (α = 0-, 6-, and 9-degree) were used to investigate the effect of the incident shock wave on unstart.	cache/02870v8624p.txt	txt/02870v8624p.txt