ON THE RESPONSE OF SHOCK-INDUCED SEPARATION BUBBLE TO SMALL AMPLITUDE DISTURBANCES

DOI10.1142/S0217984905009742zbMath1137.76409OpenAlexW2148717681MaRDI QIDQ5291509

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Publication date: 10 May 2006

Published in: Modern Physics Letters B (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0217984905009742

zbMATH Keywords

transition to turbulenceshock/boundary-layer interactions

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05)

Related Items (3)

On the length scales of hypersonic shock-induced large separation bubbles near leading edges ⋮ The effect of Mach number on unstable disturbances in shock/boundary-layer interactions ⋮ Direct numerical simulation of jets in cross-flow

Cites Work

• Entropy splitting for high-order numerical simulation of compressible turbulence
• Two-dimensional numerical investigations of small-amplitude disturbances in a boundary layer at Ma=4.8: Compression corner versus impinging shock wave

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