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

来源：

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY | 2020年 / 45卷 / 33期

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

页码：16799 / 16815

页数：17

共 130 条

[71]

McClinton CR, 2002, 26 JANNAF AIR BREATH

[72] Effect of ramp-cavity on hydrogen fueled scramjet combustor [J].

Moorthy, J. V. S. ;

Rajinikanth, B. ;

Charyulu, B. V. N. ;

Rao, G. Amba Prasad .

PROPULSION AND POWER RESEARCH, 2014, 3 (01) :22-28

[73] Shape effect of cavity flameholder on mixing zone of hydrogen jet at supersonic flow [J].

Moradi, Rasoul ;

Mahyari, A. ;

Gerdroodbary, M. Barzegar ;

Abdollahi, A. ;

Amini, Younes .

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2018, 43 (33) :16364-16372

[74] Fuel injection location studies on pylon-cavity aided jet in supersonic crossflow [J].

Oamjee, Aryadutt ;

Sadanandan, Rajesh .

AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 92 :869-880

[75] Effects of injection angle and pressure on mixing performance of fuel injection via various geometries for upstream-fuel-injected scramjets [J].

Ogawa, Hideaki .

ACTA ASTRONAUTICA, 2016, 128 :485-498

[76] Effect of variation of hydrogen injection pressure and inlet air temperature on the flow-field of a typical double cavity scramjet combustor [J].

Pandey, K. M. ;

Choubey, Gautam ;

Ahmed, Fayez ;

Laskar, Dilbahar Hussain ;

Ramnani, Pushpdeep .

INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2017, 42 (32) :20824-20834

[77]

Pandey KM, 2016, J APPL FLUID MECH, V9, P1215

[78] COMPUTATIONAL ANALYSIS OF HYPERSONIC COMBUSTOR USING STRUT INJECTOR AT FLIGHT MACH 7 [J].

Pandey, K. M. ;

Roga, S. ;

Choubey, Gautam .

COMBUSTION SCIENCE AND TECHNOLOGY, 2015, 187 (09) :1392-1407

[79]

Povinelli L., 1974, NASA TECHNICAL NOTE

[80] A novel method for flame stabilization in a strut-based scramjet combustor [J].

Qin, Qiongyao ;

Agarwal, Ramesh ;

Zhang, Xiaobing .

COMBUSTION AND FLAME, 2019, 210 :292-301

← 3 4 5 6 7 8 9 10 11 12 →