Transonic flows through cascades

  • W. Haase
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 218)


The present finite volume code for solving the Navier-Stokes equations for compressible, turbulent flows has been applied to cascade flow problems. The SKG 2.7 cascade serves as a test case with transonic — supercritical — flow conditions. The computed results seem to be in good agreement with the measurements.


Transonic Flow Surface Pressure Distribution Thin Layer Approximation Artificial Dissipation Finite Volume Technique 
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  1. [1]
    W. Haase, B. Wagner, A. Jameson: Development of a Navier-Stokes Method Based on a Finite Volume Technique for the Unsteady Euler Equations. Proceedings of the 5th GAMM-Conference on Numerical Methods in Fluid Mechanics, 1983, Notes on Numerical Fluid Dynamics, Vol. 7, M. Pandolfi/R. Piva (Ed.), Vieweg Verlag (1984)Google Scholar
  2. [2]
    A. Jameson, W. Schmidt, E. Turkel: Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Schemes. AIAA-81-1259 (1981)Google Scholar
  3. [3]
    B. S. Baldwin, H. Lomax: Thin Layer Approximation and Algebraic Model for Separated Flows. AIAA-78-257 (1978)Google Scholar
  4. [4]
    SKG-2.7-Measurements (Measurement-No. 147) provided by DFVLR, Institut für Antriebstechnik, KölnGoogle Scholar
  5. [5]
    W. Haase, K. Misegades, M. Naar: Adaptive Grids in Viscous Flow. Third Int. Conference on Numerical Methods in Laminar and Turbulent Flow, University of Washington, Seattle (1983)Google Scholar

Copyright information

© Springer-Verlag 1985

Authors and Affiliations

  • W. Haase
    • 1
  1. 1.Dornier GmbH, Theoretical AerodynamicsFriedrichshafen 1Germany

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