Shock Tunnel Investigations on Hypersonic Impinging Shock Wave Boundary Layer Interaction
The interaction of a shock wave and boundary layer often occurs in high speed flows. For sufficiently strong shock strengths the boundary layer separates, generating shock patterns in the contiguous inviscid flow (termed strong interactions); which may also affect the performances of the systems whe...
Main Author: | Sriram, R |
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Other Authors: | Jagadeesh, G |
Language: | en_US |
Published: |
2018
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Subjects: | |
Online Access: | http://etd.iisc.ernet.in/2005/3401 http://etd.iisc.ernet.in/abstracts/4267/G25866-Abs.pdf |
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