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Computation of viscous unsteady compressible flow about airfoils

  • K. Dortmann
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 323)

Keywords

Strouhal Number Lift Coefficient Vortex Street Edge Separation AIAA 13th Aerospace 
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References

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    Schweitzer, B., Krause, E., Ehrhardt, G.: Experimentelle Untersuchung instationdrer Tragflügel-strömungen. Abhandlungen aus dem Aerodynimischen Institut, RWTH Aachen, Heft 27, 1985.Google Scholar
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    Hall, M. G.: Cell-vertex multigrid schemes for solution of the Euler equations. Numerical Methods for Fluid Dynamics II. Edited by K. W. Morton and M. J. Baines, Clarendon Press, Oxford 1986.Google Scholar
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    Pulliam, T. H.: Euler and thin-layer Navier-Stokes codes: ARC2D, ARC3D. Notes for Computational Fluid Dynamics User's Workshop, University of Tennessee, Space Institute Tullahoma, March 1984.Google Scholar
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    Jameson, A., Schmidt, W., Turkel, E.: Numerical solution of the Euler equations by finite-volume methods using Runge-Kutta Time-Stepping Schemes. AIAA-81-1959.Google Scholar
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    Radespiel, R., Kroll, N.: Progress in the development of an efficient finite-volume code for the threedimensional Euler equations. DFVLR, April 1985.Google Scholar
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    Rossow, C.: Comparison of cell centered and cell vertex finite-volume schemes. Held at the 7th GAMM Conference of Numerical Methods in Fluid Mechanics. Dauvain-La-Neuve, 1987.Google Scholar
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    MacCormack, It. W., Baldwin, B. S.: A numercial method for solving the Navier-Stokes equations with applications to shock-boundary layer interactions. AIAA Paper 75-1, presented at AIAA 13th Aerospace Sciences Meeting, Pasadena, Calif., Jan. 1975Google Scholar

Copyright information

© Springer-Verlag 1989

Authors and Affiliations

  • K. Dortmann
    • 1
  1. 1.Aerodynamisches Institut, RWTH AachenAachen

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