Research in the UK on Finite Difference Methods for Computing Steady Transonic Flows
- 1 January 1976
- book chapter
- Published by Springer Nature
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- Design of Supercritical AerofoilsAeronautical Quarterly, 1974
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- Computer simulation of shock wave boundary layer interactionCommunications on Pure and Applied Mathematics, 1973
- Numerical calculation of transonic flow about swept wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Analysis of transonic airfoilsCommunications on Pure and Applied Mathematics, 1971
- The numerical calculation of steady transonic flows past thin liftingairfoils and slender bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- Calculation of plane steady transonic flowsAIAA Journal, 1971