Effect of Fuel Injection Allocation on the Combustion Characteristics of a Cavity-Strut Model Scramjet-Reference-Cited by-同舟云学术

Effect of Fuel Injection Allocation on the Combustion Characteristics of a Cavity-Strut Model Scramjet

Published:2015-01 Issue:1 Volume:28 Page:04014050
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zong Youhai¹,Bao Wen²,Chang Juntao³,Hu Jichao¹,Yang Qingchun¹,Song Jian¹,Wu Meng³

Affiliation:

1. Ph.D. Candidate, Harbin Institute of Technology, Harbin, Heilongjiang 150001, China.

2. Professor, Harbin Institute of Technology, Harbin, Heilongjiang 150001, China (corresponding author).

3. Associate Professor, Harbin Institute of Technology, Harbin, Heilongjiang 150001, 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.1943-5525.0000374

Reference40 articles.

1. Bagg C. M. G. and Greendyke R. (2009). “Computational analysis of strut induced mixing in a scram-jet.” AIAA Paper 2009-1253 American Institute of Aeronautics and Astronautics (AIAA) Reston VA.

2. Combustion characteristic using O2-pilot strut in a liquid-kerosene-fueled strut-based dual-mode scramjet

3. Effects of strut swept angle on the drag of scramjet

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

5. Cain T. and Walton C. (2002). “Review of experiments on ignition and flameholding in supersonic flow.” AIAA Paper 2002-3877 American Institute of Aeronautics and Astronautics (AIAA) Reston VA.

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