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)


Fine Mesh AIAA Paper Surface Grid Dissipation Parameter Euler Solution 
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  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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