Funder
Deutsche Forschungsgemeinschaft
TU München
GENCI
Leibniz-Rechen-zentrum München
Reference45 articles.
1. Shock pattern in the plume of rocket nozzles: needs for design consideration;Hagemann;Shock Waves,2008
2. Appearance of restricted shock separation in rocket nozzles;Hagemann;J. Propuls. Power,2002
3. Numerical simulation of rocket engine internal flows;Shimizu,2002
4. Transient three-dimensional analysis of nozzle side load in regeneratively cooled engines;Wang,2005
5. Numerical simulation of separated cold gas nozzle flows;Gross;J. Propuls. Power,2004
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