Oblique-mode breakdown and secondary instability in supersonic boundary layers
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Publication:4319580
DOI10.1017/S0022112094001965zbMath0814.76040OpenAlexW2119497073MaRDI QIDQ4319580
Mujeeb R. Malik, Chau-Lyan Chang
Publication date: 16 February 1995
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/s0022112094001965
laminar-turbulent transitionstreamwise vortexflat-plate boundary layerlow supersonic Mach numberswave-vortex triad
Parallel shear flows in hydrodynamic stability (76E05) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)
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Cites Work
- Accurate numerical solution of compressible, linear stability equations
- Analysis of the linear stability of compressible boundary layers using the PSE
- Direct numerical simulation of laminar breakdown in high-speed, axisymmetric boundary layers
- Spatial direct numerical simulation of boundary-layer transition mechanisms: Validation of \(\mathbf{PSE}\) theory
- Numerical methods for hypersonic boundary layer stability
- Effect of heat transfer on the subharmonic instability of compressible boundary layers
- Secondary instabilities in compressible boundary layers
- Secondary instability of high-speed flows and the influence of wall cooling and suction
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