Rocket Engine Nozzle Side Load Transient Analysis Methodology- a Practical Approach
Author:
Affiliation:
1. The Boeing Company
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-1860
Reference6 articles.
1. Terhardt, M.,Gagermann,G.and Frey,M."Flow separationandside-loadbehavioroftruncatedideal rocketnozzles",AIAA2001-3686,July,2001
2. Watanabe,Y.,Sakazume, N.,and Tsuboi, M. "LE-7A enginenozzleproblems duringthe transient operations",AIAA2002-3841, July2002
3. Nave, L.H.,and. Coffey,G.A, "Sea levelside loads inhigh-area-ratiorocketengine",AIAA73-1284, Nov.1973
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