Stability of three-dimensional supersonic boundary layers

DOI10.1063/1.858123zbMath0735.76027OpenAlexW1972586581MaRDI QIDQ3985663

Helen L. Reed, Ponnampalam Balakumar

Publication date: 27 June 1992

Published in: Physics of Fluids A: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1063/1.858123

zbMATH Keywords

stabilityrotating conesupersonic boundary layerscross-flow instabilityCebeci-Keller box schemetwo- point fourth-order finite-difference scheme

Mathematics Subject Classification ID

Transonic flows (76H05) Parallel shear flows in hydrodynamic stability (76E05) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (3)

Boundary layer transition and linear modal instabilities of hypersonic flow over a lifting body ⋮ Secondary instability analysis of crossflow on a hypersonic yawed straight circular cone ⋮ Linear instability of a supersonic boundary layer over a rotating cone

Cites Work

• Accurate numerical solution of compressible, linear stability equations
• Compressible boundary-layer stability theory
• The neutral curve for stationary disturbances in rotating-disk flow
• Stability of the compressible laminar boundary layer
• On the stability of three-dimensional boundary layers with application to the flow due to a rotating disk

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