Numerical study of a scramjet engine flow field
- 12 January 1981
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Numerical investigation of the perpendicular injector flow field in a hydrogen fueled scramjetPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Critical influence of finite rate chemistry and unmixedness on ignition and combustion of supersonic H2-air streamsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979