Turbulent boundary-layer interaction with a shock wave at a compression corner

DOI10.1017/S0022112084001245zbMath0592.76098MaRDI QIDQ3722111

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Publication date: 1984

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

zbMATH Keywords

matched asymptotic expansionsshock wavevelocity defect lawattached turbulent boundary layermean turbulent profilesshallow compression corner

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Existence, uniqueness, and regularity theory for compressible fluids and gas dynamics (76N10) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

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Distortion of a flat-plate boundary layer by free-stream vorticity normal to the plate ⋮ Break-away separation for high turbulence intensity and large Reynolds number ⋮ Shock-wave laminar boundary-layer interaction in supercritical transonic flow

Cites Work

• Interaction between a normal shock wave and a turbulent boundary layer at high transonic speeds. I: Pressure distribution
• Interaction between a normal shock wave and a turbulent boundary layer at high transonic speeds. II: Wall shear stress
• Interaction Between a Shock Wave and a Turbulent Boundary Layer in Transonic Flow
• On the Lagerstrom Mathematical Model for Viscous Flow at Low Reynolds Number
• The Linear‐Perturbation Theory for Rotational Flow

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