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Aerodynamic optimization of hypersonic blunted waveriders based on symbolic regression 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 卷号: 144, 页码: 18./通讯作者:Liu, Wen
Authors:  Guo SQ(郭帅旗);  Liu W(刘文);  Zhang CA(张陈安);  Liu Y(刘洋);  Wang FM(王发民)
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Hypersonic waverider  Aerodynamic model  Symbolic regression  Bluntness effect  
Influence of Non Uniform Bluntness on Aerodynamic Performance and Aerothermal Characteristics of Waverider 期刊论文
AEROSPACE, 2023, 卷号: 10, 期号: 3, 页码: 205./通讯作者:Xiao, Y (corresponding author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China., Xiao, Y (corresponding author), Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China.
Authors:  Qu, Zhipeng;  Wang, Wanyu;  Xiao, Houdi;  Xiao Y(肖尧);  Li GL(李广利);  Cui K(崔凯)
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waverider  non uniform  hypersonic  computational fluid dynamics (CFD)  
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./通讯作者:Wang YP(汪运鹏)(1,2)
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 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./通讯作者:Li, G.
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  
Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines 期刊论文
INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5./通讯作者:Zhang, Chen-An
Authors:  Zhai J;  Zhang CA(张陈安);  Wang FM(王发民);  Zhang WW
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Hypersonic inlet  lateral spillage  waverider design method  streamline tracing technology  mass-flow ratio  
Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets 期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2013, 卷号: 56, 期号: 8, 页码: 1980-1988
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Li GL(李广利);  Qu ZP(屈志朋);  Situ M;  Cui, K (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Hypersonic  Flanking Air Inlet  Waverider  Computational Fluid Dynamics(Cfd)  
Aerodynamic characteristics research on wide-speed range waverider configuration 期刊论文
Science in China Series E-Technological Sciences, 2009, 卷号: 52, 期号: 10, 页码: 2903-2910
Authors:  Wang FM(王发民);  Ding HH(丁海河);  Lei MF(雷麦芳);  Wang FM
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Waverider Configuration  Aerodynamic Characteristics At Wide-speed Range  High Lift-to-drag Ratio  
Waverider configurations derived from general conical flowfields 期刊论文
Acta Mechanica Sinica, 2007, 卷号: 23, 期号: 3, 页码: 247-255
Authors:  Cui K(崔凯);  Zhao DX;  Yang GW(杨国伟);  Cui, K (reprint author), Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116023, Peoples R China.
Adobe PDF(649Kb)  |  Favorite  |  View/Download:920/242  |  Submit date:2009/08/03
Waverider  Hypersonic  Computational Fluid Dynamics  Navier-stokes Solver  Design  Cone