Experimental Study on the Combustion Process in a Scramjet Combustor with a Rear-Wall-Expansion Geometry-Reference-Cited by-同舟云学术

Experimental Study on the Combustion Process in a Scramjet Combustor with a Rear-Wall-Expansion Geometry

Published:2018-09 Issue:5 Volume:31 Page:04018077
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Cai Zun¹,Zhu Xiaobin²,Sun Mingbo³,Wang Zhenguo³

Affiliation:

1. Ph.D. Candidate, Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Changsha, Hunan 410073, China (corresponding author).

2. Ph.D. Candidate, Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Changsha, Hunan 410073, China.

3. Professor, Science and Technology on Scramjet Laboratory, National Univ. of Defense Technology, Changsha, Hunan 410073, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000911

Reference29 articles.

1. Investigation of supersonic combustion dynamics via 50 kHz CH* chemiluminescence imaging

2. Cavity-based flameholding for chemically-reacting supersonic flows

3. Cavity Flame-Holders for Ignition and Flame Stabilization in Scramjets: An Overview

4. Large Eddy Simulation of the fuel transport and mixing process in a scramjet combustor with rearwall-expansion cavity

5. Effect of combustor geometry and fuel injection scheme on the combustion process in a supersonic flow

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