The inviscid stability of supersonic flow past heated or cooled axisymmetric bodies

DOI10.1063/1.858427zbMath0753.76060OpenAlexW2030279331MaRDI QIDQ4019479

Peter W. Duck, Stephen J. Shaw

Publication date: 16 January 1993

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

Full work available at URL: http://hdl.handle.net/2060/19910004994

zbMATH Keywords

eigenvalue problemcurvatureboundary layerasymptotic analyseswall conditionslarge azimuthal wave-number solution

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Parallel shear flows in hydrodynamic stability (76E05) Hypersonic flows (76K05)

Related Items (3)

On transition in supersonic and hypersonic boundary layers ⋮ The effect of distributed suction/injection on the spatial linear inviscid instability of a supersonic boundary layer past a slender cone ⋮ Complex-grid spectral algorithms for inviscid linear instability of boundary-layer flows.

Cites Work

• The inviscid axisymmetric stability of the supersonic flow along a circular cylinder
• Non-axisymmetric viscous lower-branch modes in axisymmetric supersonic flows
• THE WALL JET ON AN AXISYMMETRIC BODY

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