Calculation of transonic potential flow past wing-tail-fuselage combinations using the multigrid technique
Part of the Lecture Notes in Physics book series (LNP, volume 218)
KeywordsVortex Sheet Grid Level Surface Pressure Distribution Lift Surface Freestream Mach Number
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- 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
- 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
- 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
© Springer-Verlag 1985