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Unsteady viscous supersonic flow over a short flap

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Publication:1165101
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DOI10.1007/BF01094603zbMath0486.76082MaRDI QIDQ1165101

A. V. Kazakov

Publication date: 1981

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


zbMATH Keywords

matched asymptotic expansionsoscillating platelength of flappressure difference at trailing edgeunsteady flow over short flap


Mathematics Subject Classification ID

Asymptotic approximations, asymptotic expansions (steepest descent, etc.) (41A60) Supersonic flows (76J20)


Related Items (3)

Laminar boundary layer in a swirling flow on a permeable surface ⋮ Interaction between the boundary layer and a supersonic flow when part of the wall is rapidly heated ⋮ Interaction of an unsteady three-dimensional boundary layer with a hypersonic flow near a rapidly heated section of the surface



Cites Work

  • The flow about the trailing edge of a supersonic oscillating aerofoil
  • Numerical and asymptotic solutions for the supersonic flow near the trailing edge of a flat plate at incidence
  • NUMERICAL AND ASYMPTOTIC SOLUTIONS FOR THE SUPERSONIC FLOW NEAR THE TRAILING EDGE OF A FLAT PLATE
  • Upstream propagation of unsteady disturbances in supersonic boundary layers
  • Self-induced separation
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