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On the Turbulent Viscid-Inviscid Interaction at a Wedge-Shaped Trailing Edge

  • R. E. Melnik
  • B. Grossman
Conference paper

Abstract

It is generally recognized that zonal-type methods, based on boundary-layer concepts, lead to very effective procedures for computing viscous flows at high Reynolds numbers. To achieve their full potential, these methods should account for strong-interaction effects that arise at trailing edges. The trailingedge interaction is of particular importance because of its influence on the Kutta condition, leading to large global effects on lift and drag. The present paper deals with the theoretical description of strong viscid-inviscid interaction at the trailing edge of an airfoil, when the boundary layer approaching the trailing edge is a fully developed turbulent flow.

Keywords

Logarithmic Singularity Displacement Effect Displacement Thickness Upstream Boundary Layer Formal Asymptotic Solution 
These keywords were added by machine and not by the authors. This process is experimental and the keywords may be updated as the learning algorithm improves.

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Copyright information

© Springer Science+Business Media New York 1982

Authors and Affiliations

  • R. E. Melnik
  • B. Grossman
    • 1
  1. 1.Grumman Aerospace CorporationBethpageUSA

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