Shock Wave Boundary-Layer Interactions in Laminar Transonic Flow

DOI10.2514/3.49228zbMath0283.76043OpenAlexW2061386553MaRDI QIDQ4770133

H. M. Brilliant, T. C. jun. Adamson

Publication date: 1974

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2027.42/76478

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05) Asymptotic approximations, asymptotic expansions (steepest descent, etc.) (41A60) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (6)

Transonic flow over localised heating elements in boundary layers ⋮ 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 ⋮ On the internal structure of weakly nonlinear bores in laminar high Reynolds number flow ⋮ On boundary-layer transition in transonic flow ⋮ An efficient interacting boundary layer method for supersonic flow in the transonic regime

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