Analysis of Cavity Flow and The Effects of a Rod in Crossflow
Subsonic cavity flow tests of an L/D = 3.5 cavity, with three different diameter rods in crossflow, 1/8", 3/16", and 1/4", were conducted using the High Speed Wind Tunnel in the University of Tennessee Space Institute’s Gas Dynamic Laboratory. The average Mach number flow over the dur...
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Trace: Tennessee Research and Creative Exchange
2008
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| Online Access: | http://trace.tennessee.edu/utk_gradthes/463 |