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Flow behind the boundary layer separation point in a supersonic stream

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Publication:758388
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DOI10.1007/BF01013988zbMath0269.76045MaRDI QIDQ758388

D. Kharzeev

Publication date: 1973

Published in: Fluid Dynamics (Search for Journal in Brave)



Mathematics Subject Classification ID

Boundary-layer theory, separation and reattachment, higher-order effects (76D10) Supersonic flows (76J20)


Related Items (5)

Separation zones in the flow near a small-angle convex corner ⋮ Hypersonic flow over spherically blunted double cones ⋮ Temperature factor effect on the structure of the separated flow within a supersonic gas stream ⋮ The structure of a viscous fluid flow near a rotating disk edge ⋮ Break-away separation for high turbulence intensity and large Reynolds number



Cites Work

  • Unnamed Item
  • Self-induced separation
  • COMPRESSIBLE FREE SHEAR LAYER WITH FINITE INITIAL THICKNESS


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