Effect of Tube Geometry on Regenerative Cooling Performance
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Publisher
American Institute of Aeronautics and Astronautics
Reference5 articles.
1. 3Anderson,W.E.,Wennerberg,J.,Heister,S.Meyer,S.,Jung,H.andMerkle,C.L."SupercriticalFlowsinHigh Aspect Ratio Cooling Channels," AIAAPaper 2005-4302,41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Tucson, AZ, July10-13, 2005.
2. 9Carlile, J., and Quentmeyer, R. "An Experimental Investigation of High Aspect-Ratio Cooling Passages," AIAA Paper 92-3154, AIAA/SAE/ASME/ASEE 28thJoint Propulsion Conference and Exhibit, Nashville, TN .,July 6-8, 1992.
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