Influence of wall curvature on evolution of converged flow generated by crossing shock wave/boundary layer interaction: An experimental study

Author:

Zhao Yi-longORCID,Zhou Yong-yiORCID,Wang Li-canORCID,Zhao Yu-xinORCID,He Gang

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference43 articles.

1. Boundary-layer viscous correction method for hypersonic forebody/inlet integration;Ding;Acta Astronaut.,2021

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3. Fifty years of shock-wave/boundary-layer interaction research: what next?;Dolling;AIAA J.,2001

4. Advances in CFD prediction of shock wave turbulent boundary layer interactions;Knight;Prog. Aero. Sci.,2003

5. Progress in shock wave/boundary layer interactions;Gaitonde;Prog. Aero. Sci.,2015

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