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Parameters for evaluating the efficiency of inlet compression 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:  Chen, Keting;  Yue, Lianjie;  Zhang, Xinyu
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Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
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Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Advances in plasma-assisted ignition and combustion for combustors of aerospace engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 27
Authors:  Li, Mengzhe;  Wang, Zhikai;  Xu, Rongguang;  Zhang, Xiaoliang;  Chen, Zhitong;  Wang Q(汪球)
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Non-equilibrium plasma  Plasma-assisted ignition  Plasma-assisted combustion  Aerospace engine  Combustor  Extreme condition  
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
Authors:  Jiang ZL(姜宗林);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Wang C(王春);  Luo ZT(罗长童)
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Concept demonstration  Hypersonic propulsion  Oblique detonation engine  Scramjet  Shock wave  Supersonic combustion  Wind tunnel test  
Formation of stabilized oblique detonation waves in a combustor 期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:  Zhang ZJ(张子健);  Wen, Chihyung;  Zhang WS(张文硕);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Oblique detonation wave  Combustor  Oblique detonation engine  Normal detonation wave  Boundary layer separation  
Numerical investigation of a Mach 9 oblique detonation engine with fuel pre-injection 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 105, 页码: 9
Authors:  Zhang ZJ(张子健);  Ma KF(马凯夫);  Zhang WS(张文硕);  Han X(韩鑫);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
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Oblique detonation engine  Pre-injection  Detonative combustion  Mixing  Hydrogen  
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
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Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency  
Triaxial behavior of granular material under complex loading path by a new numerical true triaxial engine 期刊论文
ADVANCED POWDER TECHNOLOGY, 2019, 卷号: 30, 期号: 4, 页码: 700-706
Authors:  Wang XL(王晓亮);  Zhang Z(张珍);  Li JC(李家春)
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Granular material  Stress path  Strength criterion  Discrete element method  Numerical true triaxial engine  
Influence of integration formulations on the performance of the fast inertial relaxation engine (FIRE) method 期刊论文
COMPUTATIONAL MATERIALS SCIENCE, 2019, 卷号: 156, 页码: 135-141
Authors:  Shuang F(双飞);  Xiao P(肖攀);  Shi RH;  Ke FJ(柯孚久);  Bai YL(白以龙)
View  |  Adobe PDF(5768Kb)  |  Favorite  |  View/Download:178/21  |  Submit date:2019/04/11
Energy minimization  Fast inertial relaxation engine method  Integration formulations  Molecular simulations  
Optimization Design and Performance Analysis of a Miniature Stirling Engine 会议论文
2nd International Conference on Materials Science, Resource and Environmental Engineering (MSREE), Wuhan, PEOPLES R CHINA, OCT 27-29, 2017
Authors:  You ZP;  Yang B;  Pan LS(潘利生);  Hao CS;  You, ZP (reprint author), Shijiazhuang Tiedao Univ, Coll Mech Engn, Shijiazhuang 050043, Hebei, Peoples R China.
View  |  Adobe PDF(155Kb)  |  Favorite  |  View/Download:118/35  |  Submit date:2018/01/16
Miniature Stirling Engine  Isothermal Analysis  Adiabatic Analysis