Flame Interaction Characteristics in Scramjet Combustor Equipped with Strut/Wall Combined Fuel Injectors-Reference-Cited by-同舟云学术

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Flame Interaction Characteristics in Scramjet Combustor Equipped with Strut/Wall Combined Fuel Injectors

Published:2019-06-10 Issue:10 Volume:192 Page:1863-1886
ISSN:0010-2202
Container-title:Combustion Science and Technology
language:en
Short-container-title:Combustion Science and Technology

Author:

Zhang Junlong¹,Chang Juntao²,Tian Huimin¹,Li Ji¹,Bao Wen¹

Affiliation:

1. School of Energy Science and Engineering, Harbin Institute of Technology, Harbin, Heilongjiang, People’s Republic of China

2. Academy of Fundamental and Interdisciplinary Sciences, Harbin Institute of Technology, Harbin, Heilongjiang, People’s Republic of China

Funder

National Natural Science Foundation of China

Publisher

Informa UK Limited

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Link

https://www.tandfonline.com/doi/pdf/10.1080/00102202.2019.1627342

Reference39 articles.

1. Computational Analysis of Strut Induced Mixing in a Scramjet

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

3. Effects of upstream strut on the combustion of liquid kerosene in a model cavity scramjet

4. Evaporation and ignition of droplets in combustion chambers modeling and simulation

5. Numerical analysis and design optimization of supersonic after-burning with strut fuel injectors for scramjet engines

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1. Investigation on the effect of the leading angle of the strut on the stabilization characteristics of lifted jet flames;Acta Astronautica;2024-11

2. Numerical simulation of charged characteristics of scramjet combustion products;Aerospace Science and Technology;2024-04

3. Numerical study on the kerosene deflection characteristics and regulation methods of supersonic combustor equipped with a 75° swept strut;Acta Astronautica;2024-03

4. Numerical Investigation on Combustion Performance Optimization with Strut/Wall Combined-Staged Injection Strategy within an Axisymmetric Variable Geometry Combustor at Mach 3;2024

5. A scheme of combustion organization with combination of cone-strut and plasma torch/ oxygen addition in round supersonic combustor;Acta Astronautica;2023-11

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