Temperature factor effect on the structure of the separated flow within a supersonic gas stream
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Publication:532246
DOI10.1134/S0015462808050049zbMath1210.76104MaRDI QIDQ532246
L. A. Sokolov, V. Ya. Nejland, V. V. Shvedchenko
Publication date: 26 April 2011
Published in: Fluid Dynamics (Search for Journal in Brave)
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Related Items (2)
Bluntness and incidence effects in hypersonic flows with large separated regions ⋮ Hypersonic compression corner flow with large separated regions
Cites Work
- Flow behind the boundary layer separation point in a supersonic stream
- Numerical solution of the Navier-Stokes equations using variational iteration methods
- The interactive breakdown in supersonic ramp flow
- Once again on the supersonic flow separation near a corner
- Self-induced separation
- ON LAMINAR BOUNDARY LAYERS NEAR CORNERS
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