Hydrogen fuel in scramjet engines - A brief review

被引:167
作者
Choubey, Gautam [1 ]
Yuvarajan, D. [2 ]
Huang, Wei [3 ]
Yan, Li [3 ]
Babazadeh, Houman [4 ,5 ]
Pandey, K. M. [6 ]
机构
[1] Inst Infrastruct Technol Res & Management IITRAM, Dept Mech Engn, Ahmadabad 380026, Gujarat, India
[2] Madanapalle Inst Technol & Sci, Dept Mech Engn, Madanapalle 517325, Andhra Pradesh, India
[3] Natl Univ Def Technol, Sci & Technol Scramjet Lab, Changsha 410073, Hunan, Peoples R China
[4] Ton Duc Thang Univ, Dept Management Sci & Technol Dev, Ho Chi Minh City, Vietnam
[5] Ton Duc Thang Univ, Fac Environm & Labour Safety, Ho Chi Minh City, Vietnam
[6] Natl Inst Technol Silchar, Dept Mech Engn, Silchar, Assam, India
关键词
H-2; fuel; Scramjet engine; Mixing augmentation; Supersonic combustion; STRUT-BASED SCRAMJET; LARGE-EDDY SIMULATION; MICRO AIR-JETS; SUPERSONIC CROSS-FLOW; FLAME STABILIZATION MODES; COMBUSTION CHARACTERISTICS; CAVITY FLAMEHOLDER; MIXING AUGMENTATION; INJECTION UPSTREAM; MACH NUMBER;
D O I
10.1016/j.ijhydene.2020.04.086
中图分类号
O64 [物理化学(理论化学)、化学物理学];
学科分类号
070304 ; 081704 ;
摘要
Due to the wide flammability range and low ignition delay of Hydrogen, it can burn rapidly and generate a large amount of thrust. It is for this reason alone that many researchers have promoted hydrogen as a potential fuel in scramjet engines. As H-2 is also environmentally safe and clean and can be produced from abundant sources, several researchers across the globe support the use of H-2 fuel. However, its lower volumetric energy density and higher flammability range also have an adverse effect in on-board storage system for aircraft propulsion applications. This review gives a brief representation of Hydrogen fueled scramjet engine as well the challenges associated with H-2 fuel. Additionally, the advantage of hydrogen as a fuel as compared to other hydrocarbon fuel is also discussed here thoroughly. (C) 2020 Hydrogen Energy Publications LLC. Published by Elsevier Ltd. All rights reserved.
引用
收藏
页码:16799 / 16815
页数:17
相关论文
共 130 条
[1]   Mixing augmentation of transverse hydrogen jet by injection of micro air jets in supersonic crossflow [J].
Anazadehsayed, A. ;
Gerdroodbary, M. Barzegar ;
Amini, Y. ;
Moradi, R. .
ACTA ASTRONAUTICA, 2017, 137 :403-414
[2]  
[Anonymous], 1994, DGLR JB
[3]  
[Anonymous], 1996, SPAC PLAN HYP SYST T
[4]   Supersonic combustion of hydrogen using an improved strut injection scheme [J].
Aravind, S. ;
Kumar, Rajiv .
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2019, 44 (12) :6257-6270
[5]  
Bahman Zohuri, 2019, HYDROGEN ENERGY CHAL, DOI [10.1007/978-3-319-93461-7, DOI 10.1007/978-3-319-93461-7]
[6]   Effects of Hydrogen Fuel Injection in a Mach 12 Scramjet Inlet [J].
Barth, James E. ;
Wheatley, Vincent ;
Smart, Michael K. .
AIAA JOURNAL, 2015, 53 (10) :2907-2919
[7]  
Barth JE, 2014, AIAA SCITECH 52 AER
[8]  
Ben-Yakar A, 1998, TWENTY-SEVENTH SYMPOSIUM (INTERNATIONAL) ON COMBUSTION, VOLS 1 AND 2, P2173
[9]   Cavity flame-holders for ignition and flame stabilization in scramjets: An overview [J].
Ben-Yakar, A ;
Hanson, RK .
JOURNAL OF PROPULSION AND POWER, 2001, 17 (04) :869-877
[10]   LES of supersonic combustion in a scramjet engine model [J].
Berglund, M. ;
Fureby, C. .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2007, 31 (2497-2504) :2497-2504