Numerical Modeling of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor: Aspects of Turbulence Modeling-Reference-Cited by-同舟云学术

Numerical Modeling of Flow and Combustion in a Single-Element GCH4/GOX Rocket Combustor: Aspects of Turbulence Modeling

Published:2016-07-22 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/SAE/ASEE Joint Propulsion Conference
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Author:

Chemnitz Alexander,Sattelmayer Thomas,Roth Christof M.,Haidn Oskar J.,Daimon Yu,Keller Roman,Gerlinger Peter M.,Zips Julian,Pfitzner Michael

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4998

Reference12 articles.

1. 1Roth, C. M. “Comparison of different modeling approaches for CFD simulations of a single-element GCH4/GOX rocket combustor,” Sonderforschungsbereich/Transregio 40 { Summer Program Report 2015 , 2015.

2. 4Haidn, O., Knab, O., Celano, M., Kirchberger, C., and Schlieben, G. “Transregio SFB-TR40 - Test Case 1,” Tech. Rep. 6, Technische Universität München, Lehrstuhl für Flugantriebe, 2015.

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