A Thermal Analysis Method for Fuel-Cooled Combustor Structure based on Heat Flux Measurement
Author:
Affiliation:
1. LHD, Institute of Mechanics, Chinese Academy of Sciences
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-5878
Reference10 articles.
1. 1Wagner, W.R. and Shoji, J.M. "Advanced Regenerative Cooling Techniques for Future Space Transportation Systems," AIAA-75-1247,1975.
2. Development of Hydrocarbon-Fueled Scramjet Engines: The Hypersonic Technology (HyTech) Program
3. 3M.Traci R, L.Farr J, Jr., etal, "A Thermal Management Systems Model for the NASA GTX RBCC Concept," NASA/CR2002-211587,2002.
4. 4BouchezM,DufourE,DaniauE."Semi-empiricalandCFDAnalysisofActivelyCooledDual-modeRamjets:2006status," AIAA2006-8073,2006.
5. 5Gamble E J, Gutierrez J, Giet D, etal, "Development of a Scramjet/Ramjet Heat Exchanger Analysis Tool," AIAA 2008-4614,2008.
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