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 decoupled procedure for convection-radiation simulation in scramjets被引量：6
《Science China(Technological Sciences)》2014年第12期2551-2566,共16页WANG Jing Ying GAO Zhen Xun LEE Chun Hian ZHANG Hui Qiang 
supported by the National Natural Science Foundation of China(Grant No.11202014)
Following an order analysis of key parameters, a decoupled procedure for simulation of convection-radiation heat transfer problems in supersonic combustion ramjet(scramjet) engine was developed. The radiation module o...
关键词：SCRAMJET radiative heating convective heating turbulent combustion decoupled procedure 
Thermodynamic analysis for a chemically recuperated scramjet被引量：2
《Science China(Technological Sciences)》2012年第11期3204-3212,共9页QIN Jiang BAO Wen ZHANG SiLong SONG YuFei YU DaRen 
supported by the National Natural Science Foundation of China (General Program) (Grant No. 51106037);the Distinguished Young Scholars (Grant No. 50925625);the Innovative Research Groups(Grant No. 51121004)
Endothermic hydrocarbon fuel is regarded as an optimal fuel for a scramjet with regenerative cooling,which provides extra cooling through endothermic chemical conversion to avoid the severly limited cooling capacity w...
关键词：SCRAMJET endothermic hydrocarbon fuel chemical recuperation regenerative cooling chemical reaction 
Power generation and heat sink improvement characteristics of recooling cycle for thermal cracked hydrocarbon fueled scramjet被引量：7
《Science China(Technological Sciences)》2011年第4期955-963,共9页BAO Wen QIN Jiang ZHOU WeiXing ZHANG Duo YU DaRen 
supported by the Key Program of the National Natural Science Foundation of China (Grant No. 51076035)
In order to further investigate how much fuel heat sink could be increased and how much power generation could be obtained by using recooling cycle for a regeneratively cooled scramjet,the energy conversion from heat ...
关键词：recooling cycle SCRAMJET heat sink power generation thermal cracking 
A flamelet model for turbulent diffusion combustion in supersonic flow被引量：10
《Science China(Technological Sciences)》2010年第12期3379-3388,共10页LEE ChunHian 
In order to develop a turbulent diffusion combustion model for supersonic flow, the physical argument of the extension of the flamelet model to supersonic flow was presented, and the flow field of a hydrogen/air diffu...
关键词：SCRAMJET TURBULENT DIFFUSION COMBUSTION FLAMELET model numerical simulation 
A numerical study of turbulent combustion characteristics in a combustion chamber of a scramjet engine被引量：14
《Science China(Technological Sciences)》2010年第8期2111-2121,共11页LEE ChunHian 
3D numerical simulation of flow fields in a combustion chamber of a scramjet engine using an SST turbulence model with an explicit compressibility correction was performed and the results were compared to the experime...
关键词：SCRAMJET TURBULENT COMBUSTION FLAMELET APPROXIMATION numerical simulation 
Thermal cracking of aviation kerosene for scramjet applications被引量：20
《Science China(Technological Sciences)》2009年第9期2644-2652,共9页ZHONG FengQuan FAN XueJun YU Gong LI JianGuo 
Supported by the National Natural Science Foundation of China (Grant Nos. 10672169 and 10742003)
Thermal cracking of China No.3 aviation kerosene was studied experimentally and analytically under supercritical conditions relevant to regenerative cooling system for Mach-6 scramjet applications. A two-stage heated ...
关键词：THERMAL CRACKING AVIATION KEROSENE lumped model SCRAMJET APPLICATIONS 
Catastrophe,hysteresis and bifurcation of mode transition in scramjet engines and its model被引量：6
《Science China(Technological Sciences)》2009年第6期1543-1550,共8页YU DaRen CUI Tao BAO Wen 
Supported by the Key Program of the National Natural Science Foundation of China(Grant No.90816028)
This paper describes a class of nonlinear phenomena existing in the hypersonic flow and supersonic combustion process of scramjet engines:catastrophe,hysteresis and bifurcation,and further finds out the general rules(...
关键词：SCRAMJET ENGINE CATASTROPHE BIFURCATION MODEL 
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