A shock-fitting algorithm for the full potential equation
- 27 June 1977
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Shock-Fitting Applied to Relaxation Solutions of Transonic Small-Disturbance Equations MohammedAIAA Journal, 1977
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- RELAXATION SOLOTIONS FOR INVISCID AXISYMMETRIC TRANSOlOiC FLOW OVER BLUNT OR POINTED BODIESPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Calculation of plane steady transonic flowsAIAA Journal, 1971
- Inviscid transonic flow over airfoilsAIAA Journal, 1970