SCRAMJET

作品数：63被引量：197H指数：7
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相关领域：航空宇航科学技术更多>>
相关作者：乐嘉陵徐惊雷吴颖川王兰郑忠华更多>>
相关机构：南京航空航天大学中国空气动力研究与发展中心中国科学技术大学哈尔滨工业大学更多>>
相关期刊：《Theoretical & Applied Mechanics Letters》《Journal of Wuhan University of Technology(Materials Science)》《Chinese Journal of Mechanical Engineering》《Science Bulletin》更多>>
相关基金：国家自然科学基金国家高技术研究发展计划国家重点基础研究发展计划航天科技创新基金更多>>
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A New Method of Thermal Protection by Opposing Jet for a Hypersonic Aeroheating Strut被引量：4
《Journal of Thermal Science》2017年第3期282-288,共7页QIN Jiang NING Dongpo FENG Yu ZHANG Junlong FENG Shuo BAO Wen 
supported by Program(Nos.51476044 and 51606051);Innovative Research Groups (No.51421063) of National Natural Science Foundation of China etc
This paper presents the numerical investigation of thermal protection of scramjet strut by opposing jet in supersonic stream of Mach number 6 with a hydrogen fueled scramjet strut model using CFD software. Simulation ...
关键词：thermal protection scramjet strut opposing jet 
System Design and Analysis of Hydrocarbon Scramjet with Regeneration Cooling and Expansion Cycle被引量：8
《Journal of Thermal Science》2015年第4期350-355,共6页WU Xianyu YANG Jun ZHANG Hua SHEN Chibing 
National Natural Science Foundation of China(No.11272344)
A new expansion cycle scheme of the scramjet engine system including a hydrocarbon-fuel-based(kerosene)regenerative cooling system and supercritical/cracking kerosene-based turbo-pump was proposed in this paper.In thi...
关键词：SCRAMJET supercritical/cracking hydrocarbon regenerative cooling expansion cycle 
Experimental Study on Measurement and Calculation of Heat Flux in Supersonic Combustor of Scramjet被引量：5
《Journal of Thermal Science》2015年第3期254-259,共6页ZHANG Cong YAO Zhanli QIN Jiang BAO Wen 
An experimental measurement and calculation method which consist of thermal response model, convergence criteria and control algorithms, is proposed in this paper for the determination of heat flux in a scramjet combu...
关键词：SCRAMJET Heat flux Thermal response model Thermal protection 
Supersonic Cavity Based Combustion with Kerosene/Hydrogen Fuel
《Journal of Thermal Science》2015年第2期164-172,共9页Rajarshi Das Jeong Soo Kim Heuy Dong Kim 
supported by Advanced Research Center Program(No.2013073861) through the National Research Foundation of Korea
A comparative study with kerosene and hydrogen fuel in a model scramjet combustor has been carried out nu- merically. The effect of fuel-air equivalence ratio on the flow field properties in a cavity based mixing mech...
关键词：SCRAMJET fuel-air mixing KEROSENE HYDROGEN equivalence ratio 
Skin Friction Gage for Measurements in Hypersonic Flow
《Journal of Thermal Science》2003年第1期44-50,共7页Francois Falempin Marat Goldfeld Roman Nestoulia 
A description and results of tests of a new small-scale gage for direct measurement of skin friction force are presented in the paper.The gage design provides separated measurement of longitudinal and transversal comp...
关键词：skin friction gage hypersonic flow scramjet. 
The Effect of Injection Angle on Mixing and Flame Holding in Supersonic Combustor
《Journal of Thermal Science》2002年第1期80-91,共12页Shakil Ahmed Mohammad Ali A. K. M. Sadrul Islam 
A numerical study on mixing of hydrogen injected into a supersonic air stream has been performed by solving two-dimensional full Navier-Stokes equations. An explicit Harten-Yee Non-MUSCL Modified-flux-type TVD scheme ...
关键词：SCRAMJET engine TVD scheme backward-facing step SUPERSONIC MIXING SUPERSONIC stream flame holding. 
Preliminary Investigation of Full Model of Two-Mode Scramjet
《Journal of Thermal Science》2001年第2期97-102,共6页J.L.Le M.A.Goldfeld 等 
In this paper results of previous researches of two-mode full engine model for Mach number range from 3 to 6 are presented. The main aims of researches are to obtain characteristics of full engine model and its compon...
关键词：full engine hypersonic flow FUEL INLET COMBUSTION wind tunnel experiment. 
An Experimental Study on Transverse Hydrogen Gas Injection into Mach 1.8 Airnow Channel-The lst report:Single Circular Injector
《Journal of Thermal Science》1997年第3期207-217,共11页T.Nagashima Y.Kotani 等 
Experimental results from a series of injection tests of pressurized H2, N2 gases into Mach 1.8 airfiows between parallel channel walls through a flush-mounted circular sonic opening have been presented.Schlieren pict...
关键词：SCRAMJET supersonic combustion hydrogen transverse injection 
An Experimental Study on Transverse Hydrogen Gas Injection into Mach 1.8 Airflow Channel—The 2nd report:Tandem Circular Injectors
《Journal of Thermal Science》1997年第3期218-228,共11页T.Nagashima Y.Kotani 等 
Hydrogen gas has been injected transversely into Mach 1.8 airflow between parallel channel walls from two circular sonic injectors which were mounted flush and placed in tandem along the centre line of the bottom wall...
关键词：SCRAMJET SUPERSONIC combustion hydrogen transverse injection 
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