Appearance of Restricted Shock Separation in Rocket Nozzles
- 1 May 2002
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 18 (3), 577-584
- https://doi.org/10.2514/2.5971
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- Shock Wave Reflection PhenomenaPublished by Springer Science and Business Media LLC ,1992
- Sea level side loads in high-area-ratio rocket enginesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN OVER-EXPANDED CONICAL EXHAUST NOZZLESAIAA Journal, 1963