Experimental study of a flush wall scramjet combustor equipped with strut/wall fuel injection

Acta Astronautica ◽

10.1016/j.actaastro.2014.07.012 ◽

2014 ◽

Vol 104 (1) ◽

pp. 84-90 ◽

Author(s):

Jichao Hu ◽

Juntao Chang ◽

Wen Bao ◽

Qingchun Yang ◽

John Wen

Keyword(s):

Experimental Study ◽

Fuel Injection ◽

Scramjet Combustor

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Experimental Study on Effects of Fuel Injection on Scramjet Combustor Performance

Chinese Journal of Aeronautics ◽

10.1016/s1000-9361(07)60072-7 ◽

2007 ◽

Vol 20 (6) ◽

pp. 488-494 ◽

Author(s):

Wu Xianyu ◽

Li Xiaoshan ◽

Ding Meng ◽

Liu Weidong ◽

Wang Zhenguo

Keyword(s):

Experimental Study ◽

Fuel Injection ◽

Scramjet Combustor

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Experimental study on two oil supplies control schemes of scramjet combustor

Fuel ◽

10.1016/j.fuel.2021.120239 ◽

2021 ◽

Vol 292 ◽

pp. 120239

Author(s):

Guiqian Jiao ◽

Wenyan Song ◽

Qiang Fu ◽

Jianping Li ◽

Pinxin Wu

Keyword(s):

Experimental Study ◽

Scramjet Combustor ◽

Control Schemes

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Experimental Study of Catalyzed Diesel Particulate Filter with Exhaust Fuel Injection System for Heavy-Duty Diesel Engines

10.4271/2014-01-1496 ◽

2014 ◽

Author(s):

Tao Tang ◽

Dongxiao Cao ◽

Jun Zhang ◽

Yan-guang Zhao ◽

Shi-jin Shuai

Keyword(s):

Experimental Study ◽

Diesel Particulate Filter ◽

Fuel Injection ◽

Injection System ◽

Particulate Filter ◽

Fuel Injection System ◽

Diesel Particulate ◽

Heavy Duty Diesel ◽

Catalyzed Diesel Particulate Filter

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

Journal of Aerospace Engineering ◽

10.1061/(asce)as.1943-5525.0000911 ◽

2018 ◽

Vol 31 (5) ◽

pp. 04018077 ◽

Author(s):

Zun Cai ◽

Xiaobin Zhu ◽

Mingbo Sun ◽

Zhenguo Wang

Keyword(s):

Experimental Study ◽

Combustion Process ◽

Rear Wall ◽

Scramjet Combustor

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Experimental study on the effect of equivalence ratio and injector position on flow structure and flame development in the scramjet combustor

Aerospace Science and Technology ◽

10.1016/j.ast.2018.08.026 ◽

2018 ◽

Vol 82-83 ◽

pp. 9-19 ◽

Author(s):

Ye Tian ◽

Xuejun Zeng ◽

Shunhua Yang ◽

Fuyu Zhong ◽

Jialing Le

Keyword(s):

Experimental Study ◽

Flow Structure ◽

Equivalence Ratio ◽

Scramjet Combustor ◽

Flame Development

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Effect of Distributed Fuel Injection on Model Scramjet Combustor Performance

AIAA Propulsion and Energy 2020 Forum ◽

10.2514/6.2020-3723 ◽

2020 ◽

Author(s):

Mithuun Kanapathipillai ◽

Minwook Chang ◽

Andrew Yu ◽

Camilo Aguilera ◽

Kenneth Yu

Keyword(s):

Fuel Injection ◽

Scramjet Combustor

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Dynamic fluid flow characteristics in the hydrogen-fuelled scramjet combustor with transverse fuel injection

Case Studies in Thermal Engineering ◽

10.1016/j.csite.2019.100448 ◽

2019 ◽

Vol 14 ◽

pp. 100448 ◽

Author(s):

S.K. Gugulothu ◽

Prabhu Kishore Nutakki

Keyword(s):

Fuel Injection ◽

Flow Characteristics ◽

Scramjet Combustor ◽

Fluid Flow Characteristics

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Preliminary experimental study on solid-fuel rocket scramjet combustor

Journal of Zhejiang University SCIENCE A ◽

10.1631/jzus.a1600489 ◽

2017 ◽

Vol 18 (2) ◽

pp. 106-112 ◽

Author(s):

Zhong Lv ◽

Zhi-xun Xia ◽

Bing Liu ◽

Li-ya Huang

Keyword(s):

Experimental Study ◽

Scramjet Combustor

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Experimental study of flame stabilization in a single-side expansion scramjet combustor with different cavity length-to-depth ratios

Acta Astronautica ◽

10.1016/j.actaastro.2020.03.034 ◽

2020 ◽

Vol 173 ◽

pp. 1-8 ◽

Author(s):

Fan Li ◽

Mingbo Sun ◽

Zun Cai ◽

Yongchao Sun ◽

Fei Li ◽

...

Keyword(s):

Experimental Study ◽

Cavity Length ◽

Flame Stabilization ◽

Scramjet Combustor ◽

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Numerical Simulation on Hypersonic Combustion of Hydrogen-Fueled Scramjet Combustor with Parallel Strut Fuel Injection at a Flight Mach Number of 7

Applied Mechanics and Materials ◽

10.4028/www.scientific.net/amm.766-767.1044 ◽

2015 ◽

Vol 766-767 ◽

pp. 1044-1049

Keyword(s):

Numerical Simulation ◽

Mach Number ◽

Numerical Investigation ◽

Fuel Injection ◽

International Space ◽

Scramjet Combustor ◽

Combustion Of Hydrogen

Removed due to plagiarism. The original was published as: Numerical Investigation of Inlet-Combustor Interactions for a Scramjet Hydrogen-Fueled Engine at a Flight Mach number of 8. Authors: Edder Rabadan and Bernhard Weigand 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 2012. Paper ID AIAA-2012-5926, DOI: 10.2514/6.2012-5926

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