Shock Wave-boundary Layer Interaction in Supersonic Flow over Compression Ramp and Forward-Facing Step

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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Bibliographic Details
Main Author: Jayaprakash Narayan, M
Other Authors: Govardhan, Raghuraman N
Language:en_US
Published: 2018
Subjects:
Shock Wave-Boundary Layer Interactions
High speed vehicles
Supersonic Flow
Compression Ramp
Forward-Facing Step
Surface Flow Visualization
Particle Image Velocimetry
High-speed Schlieen Visualization
Shock Waves
Boundary Layer
SWBLIs
Shock Motions
Fluid Mechanics
Online Access:http://hdl.handle.net/2005/3014
http://etd.ncsi.iisc.ernet.in/abstracts/3861/G26746-Abs.pdf

Internet

http://hdl.handle.net/2005/3014
http://etd.ncsi.iisc.ernet.in/abstracts/3861/G26746-Abs.pdf

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