Numerical Simulation of Ignition Process in Multi-cavity Combustors at High Supersonic Flight Condition-Reference-Cited by-同舟云学术

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Numerical Simulation of Ignition Process in Multi-cavity Combustors at High Supersonic Flight Condition

Published:2017-03-02 Issue: Volume: Page:
ISSN:
Container-title:21st AIAA International Space Planes and Hypersonics Technologies Conference
language:
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Author:

Gao Liangjie¹,Wang Lu¹,Qian Zhansen¹

Affiliation:

1. Aviation Industry Corporation of China (AVIC)

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2017-2186

Reference21 articles.

1. AIAAPaper 1986-0158,1986.

2. Non-ReactingFlow,"JournalofPropulsion andPower,Vol.30,No. 2, 2014,pp. 438-448.

3. ReactingFlow,"JournalofPropulsion andPower,Vol.31, No.1,2015,pp.79-88.

4. 4Wang,Z.,Wang,H.,andSun,M."ReviewofCavity-StabilizedCombustionforScramjetapplications,"ProcIMechEPartG:

5. JAerospaceEngineering,Vol.288, No. 14,2014, pp.2718-2735.

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