Shock Wave-boundary Layer Interaction in Supersonic Flow over Compression Ramp and Forward-Facing Step
Shock wave-boundary layer interactions (SWBLIs) have been studied ex-tensively due to their practical importance in the design of high speed ve-hicles. These interactions, especially the ones leading to shock induced separation are typically unsteady in nature and can lead to large fluctuating pressu...
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Language: | en_US |
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2018
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Online Access: | http://hdl.handle.net/2005/3014 http://etd.ncsi.iisc.ernet.in/abstracts/3861/G26746-Abs.pdf |