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