Effect of Reynolds Number on Laminar Separation of a Supersonic Stream

DOI10.2514/3.61131zbMath0396.76040OpenAlexW1987712474MaRDI QIDQ4180027

Veer N. Vatsa, M. J. Werle, Odus R. Burggraf, Donald P. Rizzetta

Publication date: 1979

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.61131

zbMATH Keywords

NumericalSupersonic StreamReynolds NumberSupersonic FlowFlat PlateCompression WedgeInteracting Boundary-Layer and Asymptotic Triple-Deck EquationsLaminar SeparationSeparation RegionShear-Layer Thickness

Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Shear flows and turbulence (76F10)

Related Items (6)

The calculation of supersonic viscous flows using the parabolized Navier- Stokes equations ⋮ Non-Navier Stokes viscous flow computations ⋮ Global stability of supersonic flow over a hollow cylinder/flare ⋮ Laminar hypersonic leading edge separation – a numerical study ⋮ Triple-deck structure ⋮ Numerical study of bluntness effects on laminar leading edge separation in hypersonic flow

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