Large eddy simulation of combustion characteristics in a kerosene fueled rocket-based combined-cycle engine combustor-Reference-Cited by-同舟云学术

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Large eddy simulation of combustion characteristics in a kerosene fueled rocket-based combined-cycle engine combustor

Published:2016-10 Issue: Volume:127 Page:326-334
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Huang Zhi-wei,He Guo-qiang,Qin Fei,Cao Dong-gang,Wei Xiang-geng,Shi Lei

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference37 articles.

1. Operability benefits of airbreathing hypersonic propulsion for flexible access to space;Flaherty;J. Spacecr. Rocket.,2010

2. A.P. Kothari, J.W. Livingston, C. Tarpley, V. Raghavan, K.G. Bowcutt, T.R. Smith, Rocket Based Combined Cycle Hypersonic Vehicle Design for Orbital Access, AIAA Paper 2011-2338, 2011

3. M. Kodera, H. Ogawa, S. Tomioka, S. Ueda, Multi-objective Design And Trajectory Optimization Of Space Transport Systems with RBCC Propulsion Via Evolutionary Algorithms and Pseudo-spectral Methods, AIAA Paper 2014-0629, 2014

4. J. Lee, T.M. Krivanek, Design and Fabrication of the ISTAR Direct-connect Combustor Experiment at the NASA Hypersonic Tunnel Facility, AIAA Paper 2005-0611, 2005

5. Combustion characteristics of a dual-mode scramjet combustor with cavity flameholder;Micka;Proc. Combust. Inst.,2009

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