Numerical investigation of supersonic base flow with parallel injection
- 7 June 1982
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Computational meshes for boundary layer problemsPublished by Springer Nature ,2008
- A numerical solution of the supersonic flow over a rearward facing step with transverse non-reacting hydrogen injectionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Numerical Simulation of Near Wakes Utilizing a Relaxation Turbulence ModelAIAA Journal, 1980
- Experimental studies on the lip shock.AIAA Journal, 1968