Study on transient process of mode transition in a scramjet combustor with pilot hydrogen-Reference-Cited by-同舟云学术

Study on transient process of mode transition in a scramjet combustor with pilot hydrogen

Published:2018-03-08 Issue:7 Volume:42 Page:2481-2493
ISSN:0363-907X
Container-title:International Journal of Energy Research
language:en
Short-container-title:Int J Energy Res

Author:

Xue Rui¹^ORCID,Xu Minglong¹,Bai Changqing¹,Weng Chao²,Xu Chaoqi³

Affiliation:

1. State Key Laboratory for Strength and Vibration of Mechanical Structures, Shaanxi Engineering Laboratory for Vibration Control of Aerospace Structures, School of Aerospace; Xi'an Jiaotong University; 710049 Xi'an People's Republic of China

2. Tongji University; 200092 Shanghai People's Republic of China

3. The Sixth Academy of China Aerospace Science and Industry Corporation; 100080 Beijing People's Republic of China

Funder

National Natural Science Foundation of China

China Postdoctoral Science Foundation

Publisher

Wiley

Subject

Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment

Reference30 articles.

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2. Torrez SM Scholten NA Micka DJ Driscoll JF Bolender MA Doman DB Oppenheimer MW A scramjet engine model including effects of precombustion shock and dissociation 2008

3. A demonstration of mode transition in a scramjet combustor;Sullins;AIAA Paper,1991

4. Takahashi S Tanaka H Noborio D Miyashita T Mach 2 supersonic combustion with hydrocarbon fuels in a rectangular scramjet combustor 2003

5. Mechanism and control of combustion-mode transition in a scramjet engine;Kouchi;J Propuls Power,2012

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