Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets-Reference-Cited by-同舟云学术

Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets

Published:2016-05 Issue:5 Volume:54 Page:1693-1703
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Betti Barbara¹,Bianchi Daniele¹,Nasuti Francesco¹,Martelli Emanuele²

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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