Higher-Order, Finite-Difference Scheme for Three-Dimensional Transonic Flowfields about Axisymmetric Bodies
- 1 September 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (9) , 668-676
- https://doi.org/10.2514/3.57953
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- Calculation of plane steady transonic flowsAIAA Journal, 1971