Investigation of Two Dimensional Thermal Loads in the Region Near the Injector Head of a High Pressure Subscale Combustion Chamber
Author:
Affiliation:
1. German Aerospace Center (DLR), Institute of Space Propulsion
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-450
Reference11 articles.
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3. 4Negishi,H.,Kumakawa,A.,Yamanishi,N.,Kurosa,A.,Heattransfersimulationsinliquidrocketengine subscalethrust chamber, AIAA Paper, 44th AIAA/ASME/SAE/ASEE/JPConference andExhibit, 21-22 July 2008, Hartford,CT
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