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Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle 期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
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Multistage Launch Vehicle  Aerodynamic Characteristics  Shock Wave Interaction  Angle of Attack  Waverider  Boundary Layer Flow  Total Variation Diminishing  Adverse Pressure Gradient  Hypersonic Flows  Hypersonic Wind Tunnels  
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System 期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
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Two-stage to orbit  Numerical simulation  Stage separation  Hypersonic flow  Aerodynamic interference  
氨燃料吸气式变循环发动机性能分析 期刊论文
力学学报, 2022, 卷号: 54, 页码: 16
Authors:  张鑫;  陆阳;  程迪;  范学军
Adobe PDF(1309Kb)  |  Favorite  |  View/Download：272/50  |  Submit date：2022/10/17
氨  涡轮模态  预冷模态  冲压模态  当量总热沉  当量热值  
Kinetic-energy-flux-constrained model using an artificial neural network for large-eddy simulation of compressible wall-bounded turbulence 期刊论文
Journal of Fluid Mechanics, 2022, 卷号: 932, 页码: A23
Authors:  Yu ZP(于长平);  Yuan ZL;  Qi H(齐涵);  Wang JC;  Li XL(李新亮);  Chen SY
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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  
Shock wave and turbulent boundary layer interaction in a double compression ramp 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 15
Authors:  Tong FL(童福林);  Duan JY(段俊亦);  Li XL(李新亮)
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Shock wave  Turbulent boundary layer  Double compression ramp  Direct numerical simulation  
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
Adobe PDF(3919Kb)  |  Favorite  |  View/Download：353/88  |  Submit date：2021/08/30
Acoustic perturbation equations  Immersed boundary method  Flow-induced noise  Four-cylinder array  
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
Authors:  Fang SH(方思晗);  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Li RJ(李仁杰);  Li, Jing;  Zhang, Zhedian;  Liu, Yan;  Yu XL(余西龙)
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Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Combustion Characteristic and Mechanism of a Mixture Working Fluid C3H8/CO2 期刊论文
JOURNAL OF THERMAL SCIENCE, 2021, 页码: 12
Authors:  Shi Weixiu;  Pan LS(潘利生);  Jin Suyi;  Dong YH(董跃华);  Li T(李腾);  Zhao J(赵京);  Wei XL(魏小林)
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CO2-based mixture  flammability  laminar flame speed  flammable critical mixing ratio  transcritical power cycle  
Reduction of surface friction drag in scramjet engine by boundary layer combustion 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 115, 页码: 106788
Authors:  Xue, Rui;  Zheng, Xing;  Yue LJ(岳连捷);  Zhang, Qian;  He, Xin;  Yang, Jing;  Weng, Chao;  Li, Zhihao
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Boundary layer combustion  Skin-friction reduction  Supersonic combustion  Scramjet engine