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Direct simulation of breakdown to turbulence following oblique instability waves in a supersonic boundary layer

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Publication:4873105
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DOI10.1007/BF00849118zbMath0850.76248OpenAlexW4242358949WikidataQ61613102 ScholiaQ61613102MaRDI QIDQ4873105

Nikolaus A. Adams, Neil D. Sandham, Leonhard Kleiser

Publication date: 17 July 1996

Published in: Applied Scientific Research (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00849118



Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Shear flows and turbulence (76F10) Boundary-layer theory for compressible fluids and gas dynamics (76N20)


Related Items (6)

Effect of carbon content on supersonic shear-layer instability ⋮ Instability and low-frequency unsteadiness in a shock-induced laminar separation bubble ⋮ Transition scenario in hypersonic axisymmetrical compression ramp flow ⋮ Transient growth in compressible boundary layer flow ⋮ Numerical investigation of the nonlinear transition regime in a Mach 2 boundary layer ⋮ Reattachment streaks in hypersonic compression ramp flow: an input–output analysis




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