Effect of heat transfer on the stability of compressible boundary layers

DOI10.1016/0045-7930(92)90032-QzbMath0748.76048MaRDI QIDQ1192465

A. A. Al-Maaitah, Ali Hasan Nayfeh, Jamal A. Masad

Publication date: 27 September 1992

Published in: Computers and Fluids (Search for Journal in Brave)

zbMATH Keywords

constant Prandtl number formulationfirst-mode wavessecond-mode waves

Mathematics Subject Classification ID

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

Related Items (10)

On transition in supersonic and hypersonic boundary layers ⋮ Effect of flow–thermodynamics interactions on the stability of compressible boundary layers: insights from Helmholtz decomposition ⋮ Effect of pressure gradient on first mode of instability in compressible boundary layers ⋮ Prandtl number effects on the hydrodynamic stability of compressible boundary layers: flow–thermodynamics interactions ⋮ Sensitivity of high-speed boundary-layer stability to base-flow distortion ⋮ Triple-deck structure ⋮ Effect of heat transfer on the stability of compressible boundary layers ⋮ Interactions between vortical, acoustic and thermal components during hypersonic transition ⋮ A new inviscid mode of instability in compressible boundary-layer flows ⋮ Optimal heat flux for delaying transition to turbulence in a high-speed boundary layer

Cites Work

• On the inviscid acoustic-mode instability of supersonic shear flows. I: Two-dimensional waves
• Effect of heat transfer on the stability of compressible boundary layers
• Compressible boundary-layer stability theory
• Subharmonic instability of compressible boundary layers
• Nonparallel stability of two-dimensional nonuniformly heated boundary-layer flows
• Effect of pressure gradient on the stability of compressible boundary layers

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