LE-7A Engine Nozzle Problems during Transient Operations
- 7 July 2002
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA) in 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Restricted Shock Separation in Rocket NozzlesJournal of Propulsion and Power, 2000