Transonic flow computations using grid systems with block structure

  • K. D. Lee
  • P. E. Rubbert
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 141)


Grid Generation Grid Refinement Transonic Flow Collapse Edge Computational Plane 
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  1. 1.
    Thompson, J. F., Thames, F. C., and Mastin, C. M., “Automatic Numerical Generation of Body-Fitted Curvilinear Coordinate System for Field Containing any Number of Arbitrary Two-Dimensional Bodies,” Journal of Computational Physics, Vol. 15, 1974, pp. 299–319.Google Scholar
  2. 2.
    Holst, T. L., “A Fast, Conservative Algorithm for Solving the Transonic Full-Potential Equation,” Proc. of AIAA 4th Computational Fluid Dynamics Conference, Williamsburg, Va., July 1979, pp. 109–121.Google Scholar
  3. 3.
    Jameson, A., and Caughey, D. A., “A Finite Volume Method for Transonic Potential Flow Calculations,” Proc. of AIAA 3rd Computational Fluid Dynamics Conference, Albuquerque, N. M., June 1977, pp. 35–54.Google Scholar
  4. 4.
    Jameson, A., “Transonic Potential Flow Calculations using Conservation Form,” Proc. of AIAA 2nd Computational Fluid Dynamic Conference, Hartford, Conn., June 1975, pp. 148–155.Google Scholar

Copyright information

© Springer-Verlag 1981

Authors and Affiliations

  • K. D. Lee
    • 1
  • P. E. Rubbert
    • 1
  1. 1.Aerodynamics Research Unit Boeing Commercial Airplane CompanySeattle

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