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Standing oblique detonation for hypersonic propulsion: A review 期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
作者:  Jiang ZL(姜宗林)
Adobe PDF(10386Kb)  |  收藏  |  浏览/下载：32/2  |  提交时间：2024/02/26
Standing oblique detonation  Scramjet engine  Oblique detonation engine  Shock wave  Supersonic combustion  Hypersonic ramjet propulsion  
Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
作者:  Luo JX(罗家枭);  Zhang ZL(张泽林);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Zhou GX(周功喜);  Zhang SH(张森豪);  Li F(李飞);  Yu XL(余西龙);  Wu, Jie
Adobe PDF(732Kb)  |  收藏  |  浏览/下载：49/1  |  提交时间：2023/04/20
Combustion Instability  Rayleigh Scattering  Precombustion Chamber  Hybrid Propellant Rocket  Hybrid Rocket Motor  Mass Flow Rate  Convective Heat Transfer  Characteristic Velocity  Planar Laser Induced Fluorescence  Propulsion and Power  
Numerical and Experimental Study on Vertical Takeoff and Separation of the Compound Aircraft 期刊论文
IEEE ACCESS, 2022, 卷号: 10, 页码: 47597-47617
作者:  Wang D;  Hong QZ(洪启臻);  Huang X(黄鑫);  Pei XB;  Wang J
Adobe PDF(4750Kb)  |  收藏  |  浏览/下载：156/23  |  提交时间：2022/07/18
Aircraft  Aircraft propulsion  Compounds  Aerodynamics  Engines  Automotive components  Tail  Compound aircraft  CFD  vertical take-off  dynamical separation of two aircraft  
Transient buildup and dissipation of a compressed plasma shockwave in arc-discharge plasma beams 期刊论文
Plasma Sources Science and Technology, 2021, 卷号: 30, 期号: 12, 页码: 15
作者:  Zhang,Zhe;  Fu,Yifeng;  Zhang,Zun;  Lin X(林鑫);  Qi,Jiayun;  Ling,William Yeong Liang;  Tang,Haibin;  Herdrich,Georg
Adobe PDF(3997Kb)  |  收藏  |  浏览/下载：260/72  |  提交时间：2022/01/24
electric propulsion  plasma shockwave  ultra-high speed imaging  plasma compression  
Criteria for hypersonic airbreathing propulsion and its experimental verification 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
作者:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
Adobe PDF(1806Kb)  |  收藏  |  浏览/下载：280/55  |  提交时间：2021/05/17
Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Xiao Y(肖尧);  Cui K(崔凯);  Li GL(李广利);  Xu YZ(徐应洲)
浏览  |  Adobe PDF(639Kb)  |  收藏  |  浏览/下载：278/88  |  提交时间：2018/01/16
Aerodynamics  Air Engines  Aspect Ratio  Computational Fluid Dynamics  Drag  Engines  Hypersonic Aerodynamics  Lift  Lift Drag Ratio  Propulsion  Spacecraft  Vehicles  
A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
作者:  Cui K(崔凯);  Hu SC(胡守超);  Li GL;  Xiao Y(肖尧);  Situ M
浏览  |  Adobe PDF(872Kb)  |  收藏  |  浏览/下载：353/153  |  提交时间：2017/05/05
Aero  Dynamic Performance  Aerodynamic Performance Predictions  Design Methodology  Flight Altitudes  Numerical Results  Propulsion System  Turbulent Models  Wing Body Aircraft  
Investigation of the plasma flow in arcjet using continuum and dicrete approaches 会议论文
The 29th International Symposium on Rarefied Gas Dynamics, 中国陕西西安, 2014-07-13
作者:  Yang BJ(杨弼杰);  Sun QH(孙泉华)
浏览  |  Adobe PDF(28Kb)  |  收藏  |  浏览/下载：204/33  |  提交时间：2015/09/10
Downstream  Propulsion  Kinetics  Impulse  Heated  Nozzle  Continuum  Overlapped  Capture  Thrust  
Characteristics of compressible flow of supercritical kerosene 期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 1, 页码: 8-13
作者:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Wang J(王晶);  Yu G(俞刚);  Li JG(李建国);  Fan, XJ;  Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(484Kb)  |  收藏  |  浏览/下载：961/299  |  提交时间：2013/01/18
Supercritical Kerosene  Compressible Flow  Laval Nozzle  Isentropic Process  Aviation Kerosene  Combustion  Propulsion  
Heat Transfer of Aviation Kerosene at Supercritical Conditions 期刊论文
Journal of Thermophysics and Heat Transfer, 2009, 卷号: 23, 期号: 3, 页码: 543-550
作者:  Zhong FQ(仲峰泉);  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国);  Sung CJ;  Zhong FQ
Adobe PDF(674Kb)  |  收藏  |  浏览/下载：1898/710  |  提交时间：2009/08/03
Cracked Kerosene  Rocket Fuels  Combustion  Propulsion