Author:
Wennerberg Jason,Anderson William,Haberlen Philip,Jung Hogirl,Merkle Charles
Publisher
American Institute of Aeronautics and Astronautics
Reference27 articles.
1. 1Wadel, M.F. "Comparison of High Aspect Ratio Cooling Channel Designs for a Rocket Combustion Chamber with Development ofan Optimized Design", NASA-TM-206313, 1998.
2. 2Hendricks, R.C. and Simon, F.F. "Heat Transfer to Hydrogen in a Curved Tube," Presented at theASME meeting, Philadelphia, November, 1963.
3. 4Neuner,F., Preclik, D., Popp, M., Funke, M., and Kluttig, H. "Experimental and Analytical Investigation of Local Heat Transferin High-Aspect-Ratio Cooling Channels,"AIAA-98-3439,34thJointPropulsion Conference, 1998.
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