Inviscid Supersonic/Hypersonic Body Flowfield and Aerodynamicsfrom Shock-Capturing Technique Calculations
- 1 June 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 13 (6) , 325-331
- https://doi.org/10.2514/3.57094
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973
- Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference SchemesAIAA Journal, 1973
- Numerical Solution for Three-Dimensional Inviscid Supersonic FlowAIAA Journal, 1972
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969