Numerical solution for the inviscid supersonic flow in the corner formed by two intersecting wedges
- 16 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973
- Shock-Capturing, Finite-Difference Approach to Supersonic FlowsJournal of Spacecraft and Rockets, 1971
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971
- Hypersonic interaction along a rectangular cornerAIAA Journal, 1969
- Supersonic interference flow along the corner of intersecting wedges.AIAA Journal, 1967
- UNIFORMLY VALID SECOND-ORDER SOLUTION FOR SUPERSONIC FLOW OVER CRUCIFORM SURFACESAIAA Journal, 1963
- Weak solutions of nonlinear hyperbolic equations and their numerical computationCommunications on Pure and Applied Mathematics, 1954