Hypersonic Incident Shock-Boundary Layer Interaction Control by Wavy Patches-Reference-Cited by-同舟云学术

Hypersonic Incident Shock-Boundary Layer Interaction Control by Wavy Patches

Published:2021-01 Issue:1 Volume:34 Page:04020092
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Chitharenjan Ashok¹^ORCID,Menezes Viren²^ORCID

Affiliation:

1. Research Scholar, Dept. of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai, Maharashtra 400076, India (corresponding author). ORCID: .

2. Professor, Dept. of Aerospace Engineering, Indian Institute of Technology Bombay, Mumbai, Maharashtra 400076, India. ORCID: .

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001203

Reference36 articles.

1. Hypersonic and High-Temperature Gas Dynamics, Second Edition

2. Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions

3. Stationary vortices and persistent turbulence in Karman grooves

4. Berry S. A. R. J. Novak and T. J. Horvath. 2004. “Boundary layer control for hypersonic air breathing vehicles.” In Proc. 34th AIAA Fluid Dynamics Conf. Reston VA: American Institute of Aeronautics and Astronautics.

5. Stabilization of a Hypersonic Boundary Layer Using a Wavy Surface

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