Evaluation of parallel injector configurations for supersonic combustion
- 12 July 1989
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Progress toward shock enhancement of supersonic combustion processesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987