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Transonic Separated Flow Prediction Based on a Mathematically Simple, Nonequilibrium Turbulence Closure Model

  • D. A. Johnson
  • L. S. King
Conference paper
Part of the International Union of Theoretical and Applied Mechanics book series (MANUTECH)

Summary

A mathematically simple, turbulence closure model designed to treat transonic airfoil flows even with massive separation is described. Numerical solutions of the Reynolds-averaged, Navier-Stokes equations obtained with this closure model are shown to agree well with experiments over a broad range of test conditions.

Keywords

Eddy Viscosity Closure Model Reynolds Shear Stress Adverse Pressure Gradient Turbulence Closure Model 
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-Verlag Berlin, Heidelberg 1986

Authors and Affiliations

  • D. A. Johnson
    • 1
  • L. S. King
    • 1
  1. 1.NASA Ames Research CenterMoffett FieldUSA

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