Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets
Author:
Affiliation:
1. Sapienza University of Rome, 00184 Rome, Italy
2. Second University of Naples, 81031 Aversa, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J054606
Reference29 articles.
1. SuttonG. P.BiblarzO., Rocket Propulsion Elements, Wiley, New York, 2001, pp. 286–320.
2. Heat Transfer from Chemically Reacting Gases
3. SCALE EFFECTS AND CORRELATIONS IN NONEQUILIBRIUM CONVECTIVE HEAT TRANSFER
4. Turbulent Heat Transfer to a Nonequilibrium Chemically Reacting Gas
5. HowellJ. R.StriteM. K.RenkelH. E. “Analysis of Heat-Transfer Effects in Rocket Nozzles Operating with Very High-Temperature Hydrogen,” NASA TR-R-220, 1965.
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