LE-7A Engine Separation Phenomenon Differences of the Two Nozzle Configurations
- 26 June 2003
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA) in 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- LE-7A Engine Nozzle Problems during Transient OperationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2002
- Sub Scale Nozzle Combustion Tests of the LE-7A Engine for Clarification of Large Side-Loads(II)-Influence of a Step in Nozzle Contour on Side-LoadPublished by American Institute of Aeronautics and Astronautics (AIAA) ,2002
- Restricted Shock Separation in Rocket NozzlesJournal of Propulsion and Power, 2000
- Design of compressed truncated perfect nozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985