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Superior Al90Mg10-Based Composite Fuel Grain for a Hybrid Rocket Engine 期刊论文
JOURNAL OF SPACECRAFT AND ROCKETS, 2024, 页码: 9./通讯作者：Lin, Xin
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Pan JJ(潘俊杰);  Luo JX(罗家枭);  Wang RY(王若岩);  Zhang ZL(张泽林);  Yu XL(余西龙)
Favorite  |  View/Download：48/0  |  Submit date：2024/05/21
Combustion Efficiency  Emission Spectroscopy  Hybrid Rocket Engines  Paraffin Based Fuels  Regression rate  Aluminium Alloys  3D Printing  
Coupling Effect of Multicavity on Flame Stabilization Mode Transitions in Scramjet Combustor 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023./通讯作者：Zhang, QF
Authors:  Wu ZJ(吴振杰);  Zhang QF(张启帆);  Yu FY(于方游);  Luo WH(罗苇航);  Gao ZB(高占彪);  Yue LJ(岳连捷)
Adobe PDF(582Kb)  |  Favorite  |  View/Download：72/14  |  Submit date：2023/06/15
Scramjet Engines  Combustor Design  flame stabilization mode  transition  path dependence  
Charactering Catalytic Ignition and Combustion for the Ninety Percent Hydrogen Peroxide/Paraffin Based Hybrid Rocket Engine 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023./通讯作者：Wang, ZZ (corresponding author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Wu K(吴坤);  Zhang ZL(张泽林);  Fang SH(方思晗);  Meng DD(孟东东);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(712Kb)  |  Favorite  |  View/Download：144/15  |  Submit date：2023/04/20
Hybrid Rocket Engines  Propellant  Thermocouples  Numerical Analysis  Catalysis  Absorption Spectroscopy  Combustion Products  decomposition efficiency  Paraffin Fuel  Ignition Systems  
Investigation on the Flow Instability of Supercritical Hydrocarbon Fuels in Cooling Channels 期刊论文
JOURNAL OF THERMOPHYSICS AND HEAT TRANSFER, 2023./通讯作者：Fan, XJ (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China., Fan, XJ (corresponding author), Univ Chinese Acad Sci, Inst Mech, Beijing, Peoples R China.
Authors:  Jin YC(靳一超);  Wu K(吴坤);  Lu Y(陆阳);  Fan XJ(范学军)
Adobe PDF(1806Kb)  |  Favorite  |  View/Download：136/17  |  Submit date：2023/04/20
Scramjet Engines  Regenerative Cooling  Supercritical Fluid  Hydrocarbon Fuels  Flow Instability  Fluid Dynamics  
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./通讯作者：WANG, J. I. N. G.
Authors:  Wang D;  Hong QZ(洪启臻);  Huang X(黄鑫);  Pei XB;  Wang J
Adobe PDF(4750Kb)  |  Favorite  |  View/Download：234/36  |  Submit date：2022/07/18
Aircraft  Aircraft propulsion  Compounds  Aerodynamics  Engines  Automotive components  Tail  Compound aircraft  CFD  vertical take-off  dynamical separation of two aircraft  
Aerodynamic principles of shock-induced combustion ramjet engines 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 103, 页码: 8./通讯作者：Liu, Yunfeng
Authors:  Ma KF(马凯夫);  Zhang ZJ(张子健);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
Adobe PDF(1657Kb)  |  Favorite  |  View/Download：330/114  |  Submit date：2020/08/26
Scramjet engines  Shock-induced combustion ramjet engines  Supersonic combustion  Chapman-Jouguet detonation  
Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Cheng LW(程柳维);  Zhong FQ(仲峰泉);  Wang ZP(王知溥);  Gu HB(顾洪斌);  Ma SG(马素刚);  Zhang XY(张新宇)
View  |  Adobe PDF(517Kb)  |  Favorite  |  View/Download：407/123  |  Submit date：2018/01/16
Combustors  Cracks  Diesel Engines  Efficiency  Ethylene  Fighter Aircraft  Fuels  High Speed Cameras  Ignition  Kerosene  Luminance  Spacecraft  Stabilization  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng([email protected])
View  |  Adobe PDF(1249Kb)  |  Favorite  |  View/Download：378/116  |  Submit date：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
A low-dissipation solver based on openFOAM designed for large eddy simulation in compressible flow 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:  Lee YC;  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(1377Kb)  |  Favorite  |  View/Download：570/120  |  Submit date：2018/11/08
Computational Fluid Dynamics  Digital Storage  Kinetic Energy  Kinetics  Open Source Software  Open Systems  Ramjet Engines  Runge Kutta Methods  Shock Tubes  Turbulence  Two Phase Flow  Bench  Mark Problems  Central  Upwind Scheme  Computational Fluid Dynamics Software  Skew  Symmetric Forms  Temporal Discretization  Turbulence Structures  Unstructured Meshes  Wall Bounded Turbulence  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors:  Yao W(姚卫);  Fan XJ(范学军)
View  |  Adobe PDF(832Kb)  |  Favorite  |  View/Download：348/107  |  Submit date：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion