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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 KT(陈科挺);  Yue LJ(岳连捷);  Zhang XY(张新宇)
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Airbreathing engine  Compression efficiency  Compression quality  Inlet  Self-consistency  
Design of a milli-newton force balance for hypersonic rarefied wind tunnel 期刊论文
MEASUREMENT, 2021, 卷号: 185, 页码: 7
Authors:  Wu CW(吴臣武);  Liu C(刘聪);  Hu DL(胡灯亮);  Liu HL(刘宏立);  Huang HJ(黄河激)
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Strain  Balance  Milli-newton  Design  Calibration  
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  
Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 416-425
Authors:  Xie, Wei;  Luo, Zhenbing;  Zhou, Yan;  Gao, Tianxiang;  Wu, Yun;  Wang Q(汪球)
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SparkJet  High-enthalpy hypersonic flow  Shock control  Shock-on-shock interaction  Air supply  
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing 期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:  Lin MY(林明月);  Wang C(王春);  Peng J(彭俊);  Jiang ZL(姜宗林)
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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  
A sharp interface immersed boundary method for flow-induced noise prediction using acoustic perturbation equations 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 227, 页码: 15
Authors:  Zhao, Cheng;  Yang Y(杨焱);  Zhang, Tao;  Dong, Haibo;  Hou, Guoxiang
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Acoustic perturbation equations  Immersed boundary method  Flow-induced noise  Four-cylinder array  
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:  Zhou GX(周功喜);  Zhang X(张旭);  Li JP(李进平);  Zhang XY(张晓源);  Zhang SZ(张仕忠);  Lin X(林鑫);  Li F(李飞);  Chen H(陈宏);  Yue LJ(岳连捷);  Yu XL(余西龙)
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High mach number scramjet  Circular cross-section  TDLAS  Multi-view simultaneous imaging  POD  
Parametric Study on Lateral–Directional Stability of Hypersonic Waverider 期刊论文
AIAA Journal, 2021, 卷号: 59, 期号: 8, 页码: 3025-3042
Authors:  刘文;  张陈安;  Wang Xiao-Peng;  Li Jin-Jie;  王发民
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Numerical study on aerodynamic performance of waverider with a new bluntness method 期刊论文
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 卷号: 235, 期号: 10, 页码: 1225-1233
Authors:  Qu ZP;  Xiao HD;  Lv MY;  Li GL(李广利);  Cui K(崔凯)
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bluntness method  computational fluid dynamics  hypersonic  volume  Waverider