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Aerothermodynamics of Shock-Boundary Layer Interaction in Hypersonic Flow: A Study on Stagnation Pressure Loss and the Extend of Separation Zone

Publication Type : Conference Proceedings

Publisher : 3rd National Symposium on Shock Waves

Source : 3rd National Symposium on Shock Waves. IIT Bombay, 2014.

Campus : Coimbatore

School : Department of Aerospace Engineering, School of Engineering

Department : Aerospace

Verified : Yes

Year : 2014

Abstract :

Cite this Research Publication : U. Viverjita and Dr. Srikrishnan A. R., “Aerothermodynamics of Shock-Boundary Layer Interaction in Hypersonic Flow: A Study on Stagnation Pressure Loss and the Extend of Separation Zone”, 3rd National Symposium on Shock Waves. IIT Bombay, 2014.

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