Floating shock fitting for three-dimensional inviscid supersonic flows
- 1 January 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 20 (1) , 9-17
- https://doi.org/10.2514/3.7897
Abstract
No abstract availableKeywords
This publication has 12 references indexed in Scilit:
- Discretization of boundary conditions on moving discontinuitiesPublished by Springer Nature ,2008
- Floating Shock Fitting for Cones at Large IncidenceAIAA Journal, 1978
- Inviscid Flowfield Calculations for Re-entry Vehicles with Control SurfacesAIAA Journal, 1977
- Three dimensional supersonic flows with subsonic axial Mach numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Shock Fitting Method for Complicated Two-Dimensional Supersonic FlowsAIAA Journal, 1976
- Computation of nonequilibrium three-dimensional inviscid flow over blunt-nosed bodies flying at supersonic speedsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Supersonic Flow about Slab Delta Wings and Wing-Body ConfigurationsJournal of Spacecraft and Rockets, 1973
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973
- Numerical Solution for Three-Dimensional Inviscid Supersonic FlowAIAA Journal, 1972
- A complete numerical technique for the calculation of three-dimensional inviscid supersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972