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Development of a highly efficient and accurate 3D Euler flow solver

  • H. C. Chen
  • N. J. Yu
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 323)

Keywords

Fine Mesh AIAA Paper Surface Grid Dissipation Parameter Euler 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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References

  1. 1.
    Yu, N. J., Chen, H. C., Chen, A. W. and K. R. Wittenberg, “Grid Generation and Flow Code Development for Winglet Analysis,” AIAA Paper 88-2548, presented at AIAA Sixth Applied Aerodynamic Conference, June 1988.Google Scholar
  2. 2.
    Jameson, A. and Baker, T. J. “Multigrid Solution of the Euler Equations for Aircraft Configurations,” AIAA Paper 84-0093, 1984.Google Scholar
  3. 3.
    Jameson, A., “Successes and Challenges in Computational Aerodynamics,” AIAA Paper 87-1184,1987.Google Scholar
  4. 4.
    Swanson, R. C. and Turkel, E., “Artificial Dissipation and Central Difference Schemes for the Euler and Navier-Stokes Equations,” AIAA Paper 87-1107, 1987.Google Scholar
  5. 5.
    Jameson, A., Schmidt, W., and Turkel, E., “Numerical Solutions of the Euler Equations by Finite Volume Methods Using Runge-Kutta Time-Stepping Scheme,” AIAA 81-1259,1981.Google Scholar
  6. 6.
    Chen, H. C., Yu, N. J. and Rubbert, P. E., “Flow Simulations for General Nacelle Configurations Using Euler Equations,” AIAA 83-0539, 1983.Google Scholar

Copyright information

© Springer-Verlag 1989

Authors and Affiliations

  • H. C. Chen
    • 1
  • N. J. Yu
    • 1
  1. 1.Boeing Commercial AirplanesSeattle

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