LE-7A Engine Nozzle Flow Separation Phenomenon and the Possibility of RSS Suppression by the Step Inside the Nozzle
- 26 June 2004
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA) in 40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Design of compressed truncated perfect nozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985