Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas Effects
Authors:
- 1 May 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (5) , 657-664
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Numerical Solution for Three-Dimensional Inviscid Supersonic FlowAIAA Journal, 1972
- Computation of supersonic flow fields about bodies in coning motion using a shock-capturing finite-difference technique1972
- A complete numerical technique for the calculation of three-dimensional inviscid supersonic flows1972
- Comparison of characteristics and shock capturing methods with application to the space shuttle vehicle1972
- The effect of viscosity in hypervelocity impact cratering1969
- The Supersonic Flow Past an Elliptic ConeAeronautical Quarterly, 1969
- Three-dimensional flow calculation by the method of characteristics.AIAA Journal, 1967