Appearance of Restricted Shock Separation in Rocket Nozzles
Author:
Affiliation:
1. Astrium GmbH, D-81663 Munich, Germany
2. DLR, German Aerospace Center, D-74239 Hardthausen, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.5971
Reference18 articles.
1. Sea level side loads in high-area-ratio rocket engines
2. Flow separation and side-loads in rocket nozzles
3. Restricted Shock Separation in Rocket Nozzles
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