The numerical calculation of inviscid plume flow fields
- 17 June 1974
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- The Mach disc in underexpanded exhaust plumesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1970
- A CRITICAL ANALYSIS OF NUMERICAL TECHNIQUES: THE PISTON-DRIVEN INVISCID FLOWPublished by Defense Technical Information Center (DTIC) ,1969
- The effect of viscosity in hypervelocity impact crateringPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1969
- LOCATION OF THE NORMAL SHOCK WAVE IN THE EXHAUST PLUME OF A JETAIAA Journal, 1963
- CALL FOR PAPERS: XIVth International Astronautical CongressAIAA Journal, 1963