Cartesian mesh solution for axisymmetric transonic potential flow around inlets
- 14 July 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Calculation of Transonic Flow around Axisymmetric InletsAIAA Journal, 1975
- Convergence acceleration and shock fitting for transonic aerodynamics computationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- 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
- Transonic flow analysis using a streamline coordinate transformationprocedurePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Calculation of plane steady transonic flowsAIAA Journal, 1971
- Inviscid transonic flow over airfoilsAIAA Journal, 1970