Calculation of transonic potential flow past wing-tail-fuselage combinations using the multigrid technique

  • Arvin Shmilovich
  • D. A. Caughey
Contributed Papers
Part of the Lecture Notes in Physics book series (LNP, volume 218)


Vortex Sheet Grid Level Surface Pressure Distribution Lift Surface Freestream Mach Number 
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  1. 1.
    Shmilovich, A. and Caughey, D. A., “Grid Generation for Wing-Tail-Fuselage Configurations”, Advances in Grid Generation, Ghia, K. N. and Ghia, U., Eds., American Society of Mechanical Engineers, 1983, pp. 189–197.Google Scholar
  2. 2.
    Shmilovich, A. and Caughey, D. A., “Application of the Multigrid Method to Calculations of Transonic Potential Flow about Wing-Fuselage Combinations”, J. Comp. Phys., Vol. 48, 1982, pp. 462–484.CrossRefGoogle Scholar
  3. 3.
    Caughey, D. A. and Shmilovich, A., “Multigrid Calculation of Transonic Potential Flows”, Numerical Methods in Fluids: Advances in Computational Transonics, Vol. 4, Habashi, W. W., Ed., Pineridge Press, Swansea, U.K., 1984.Google Scholar
  4. 4.
    Caughey, D. A., “Multigrid Calculation of Three-Dimensional Transonic Potential Flows”, Appl. Math. and Comp., Vol. 13, 1983, pp. 241–260.CrossRefGoogle Scholar
  5. 5.
    Shmilovich, A., “Calculation of Transonic Potential Flow past Wing-Tail-Fuselage Configurations Using the Multigrid Method”, Ph.D. Thesis, Cornell University, 1983.Google Scholar

Copyright information

© Springer-Verlag 1985

Authors and Affiliations

  • Arvin Shmilovich
    • 1
  • D. A. Caughey
    • 1
  1. 1.Sibley School of Mechanical and Aerospace EngineeringCornell UniversityIthaca, NYUSA

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