Timescale-Based Frozen Nonadiabatic Flamelet Combustion Modeling for Rocket Engine Thrust Chambers
Author:
Affiliation:
1. Technical University of Munich, 85748 Garching, Germany
2. ArianeGroup GmbH, 82024 Taufkirchen, Germany
Funder
Deutsches Zentrum für Luft- und Raumfahrt
Bayerische Forschungsstiftung
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B37936
Reference45 articles.
1. Chemical Reaction Effects on Heat Loads of CH4/O2 and H2/O2 Rockets
2. The impact of methane oxidation kinetics on a rocket nozzle flow
3. Consequences of modeling demands on numerical rocket thrust chamber flow simulation tools
4. Laminar diffusion flamelet models in non-premixed turbulent combustion
5. PetersN., Turbulent Combustion, 3rd ed. Cambridge Univ. Press, Cambridge, England, U.K., 2000, pp. 170–236.
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