Theoretical liquid rocket engine nozzle flow fields
- 6 July 1992
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Advanced liquid rocket engine transient modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Characteristic-based algorithms for flows in thermo-chemical nonequilibriumPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- PARC Code: Theory and UsagePublished by Defense Technical Information Center (DTIC) ,1989
- A numerical study of chemically reacting flow in nozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Analysis tool for application to ground testing of highly underexpanded nozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987