Transonic Potential Flow around Axisymmetric Inlets and Bodies at Angle of Attack
- 1 September 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (9) , 1299-1306
- https://doi.org/10.2514/3.60786
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
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- Cartesian Mesh Solution for Axisymmetric Transonic Potential Flow Around InletsAIAA Journal, 1977
- Transonic Airfoil Analysis and Design Using Cartesian CoordinatesJournal of Aircraft, 1976
- Accelerated iterative calculation of transonic nacelle flowfieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
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- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- Analysis of Embedded Shock Waves Calculated by Relaxation MethodsAIAA Journal, 1974
- NUMERICAL CALCULATION OF THE THREE DIMENSIONAL TRANSONIC FLOW OVER A YAWED WINGPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- RELAXATION SOLOTIONS FOR INVISCID AXISYMMETRIC TRANSOlOiC FLOW OVER BLUNT OR POINTED BODIESPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Inviscid transonic flow over airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970