Sidewall influence of varying free stream Mach number in ramp induced shock wave boundary layer interactions-Reference-Cited by-同舟云学术

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Sidewall influence of varying free stream Mach number in ramp induced shock wave boundary layer interactions

Published:2024-07 Issue:4 Volume:14 Page:100541
ISSN:2095-0349
Container-title:Theoretical and Applied Mechanics Letters
language:en
Short-container-title:Theoretical and Applied Mechanics Letters

Author:

Mangalagiri Raja,Jammy Satya P^ORCID

Publisher

Elsevier BV

Reference26 articles.

1. Theoretical and experimental studies of the shock-wave boundary layer interaction on compression surfaces in hypersonic flow;Holden,1969

2. PIV measurements of hypersonic laminar flow over a compression ramp;Lu,2019

3. Shock-wave/boundary-layer interactions at compression ramps studied by high-speed schlieren;Sun;AIAA J.,2020

4. Experimental and computational investigations of hypersonic flow about compression ramps;Simeonides;J. Fluid Mech.,1995

5. Effect of freestream parameters on the laminar separation in hypersonic shock wave boundary layer interaction;Kumar;ADBU J. Eng. Technol. (AJET),2016

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