Effect of heat transfer on the stability of compressible boundary layers
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Publication:1192465
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)
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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