Experimental and Analytical Design Verification of the Dual-Bell Concept
- 1 January 2002
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 18 (1), 116-122
- https://doi.org/10.2514/2.5905
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Restricted Shock Separation in Rocket NozzlesJournal of Propulsion and Power, 2000
- A sub scale investigation on side loads in sea level rocket nozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Flow separation and side-loads in rocket nozzlesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1999
- Critical Assessment of Dual-Bell NozzlesJournal of Propulsion and Power, 1999