COMPARISON OF A DISCRETE-SHOCK, FINITE-DfFFEf^tNCi^ 1ECHNIQUE AND THE METHOD OF CHARACTERISTICS FOR CALCULATING INTERNAL SUPERSONIC FLOWS
- 19 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Application of selected finite difference techniques to the solution of conical flow problemsPublished by Iowa State University ,2018
- Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas EffectsAIAA Journal, 1973