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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
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Wang C(王春);  Jiang ZL(姜宗林)
Adobe PDF(5479Kb)  |  收藏  |  浏览/下载：363/69  |  提交时间：2022/08/24
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  
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel 期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
作者:  Wang Y(王粤);  Wang YP(汪运鹏);  Jiang ZL(姜宗林)
Adobe PDF(2434Kb)  |  收藏  |  浏览/下载：305/81  |  提交时间：2022/08/23
Aerodynamic Coefficients  Two Stage to Orbit  Aerodynamic Performance  Hypersonic Flight  Hypersonic Wind Tunnels  Solenoid Valves  Oblique Shock  Pneumatic Actuator  Hypersonic Flows  Computer Aided Engineering  
Direct numerical simulation of a supersonic turbulent boundary layer over a compression–decompression corner 期刊论文
Physics of Fluids, 2021, 卷号: 33, 页码: 065111
作者:  段俊亦;  李欣;  李新亮;  刘洪伟
Adobe PDF(5069Kb)  |  收藏  |  浏览/下载：168/41  |  提交时间：2021/11/23
Statistical characteristics of turbulent mixing in spherical and cylindrical converging Richtmyer–Meshkov instabilities 期刊论文
Journal of Fluid Mechanics, 2021, 卷号: 928, 页码: A10
作者:  李新亮;  符耀威;  于长平;  李理
Adobe PDF(3374Kb)  |  收藏  |  浏览/下载：156/36  |  提交时间：2021/11/23
Direct numerical simulation of supersonic turbulent expansion corner with shock impingement 期刊论文
Physics of Fluids, 2021, 卷号: 33, 页码: 105104
作者:  Zhang ZG(张志刚);  Tong FL(童福林);  Duan JY(段俊亦);  Li XL(李新亮)
Adobe PDF(8048Kb)  |  收藏  |  浏览/下载：141/39  |  提交时间：2021/11/23
Coupling Analysis for the Thermo-Acoustic-Vibration Response of a Thin-Walled Box with Acoustic Excitations 期刊论文
JOURNAL OF VIBRATION ENGINEERING & TECHNOLOGIES, 2016, 卷号: 4, 期号: 5, 页码: 423-429
作者:  Yang Y(杨焱);  Wu CW(吴臣武);  Wu, CW (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(733Kb)  |  收藏  |  浏览/下载：360/85  |  提交时间：2016/12/08
Thermal  Vibration  Acoustic  Multi-physics Environment  
高超声速电离绕流中电子密度的静电探针测量方法研究 期刊论文
实验流体力学, 2013, 卷号: 27, 期号: 6, 页码: 64-69+85
作者:  汪球;  赵伟;  余西龙;  姜宗林
Adobe PDF(487Kb)  |  收藏  |  浏览/下载：891/231  |  提交时间：2014/01/24
静电探针  电子密度  高超声速  高焓激波风洞  Electrostatic Probe  Electron Density  Hypersonic  High Enthalpy Shock Tunnel  
Discharge characteristics and abatement of volatile organic compounds using plasma reactor packed with ceramic Raschig rings 期刊论文
JOURNAL OF ELECTROSTATICS, 2013, 卷号: 71, 期号: 5, 页码: 939-944
作者:  Dou BJ;  Bin F(宾峰);  Wang C;  Jia QZ;  Li J;  Bin, F (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
Adobe PDF(833Kb)  |  收藏  |  浏览/下载：614/283  |  提交时间：2013/11/18
Non-thermal Plasmas  Lissajous Diagram  Discharge Parameters  Ceramic Raschig Rings  Toluene Removal  
Approximate analytic solution of heat conduction in hollow semi-spheres flying at hypersonic speed 期刊论文
INTERNATIONAL COMMUNICATIONS IN HEAT AND MASS TRANSFER, 2013, 卷号: 43, 页码: 46-52
作者:  Han GL(韩桂来);  Jiang ZL(姜宗林);  Han, GL (reprint author), Chinese Acad Sci, Stake Key Lab High Temp Gas Dynam LHD, Inst Mech, Beijing 100190, Peoples R China.
Adobe PDF(548Kb)  |  收藏  |  浏览/下载：1095/326  |  提交时间：2013/05/31
Heat Conduction  Theoretical Investigation  Approximate Solution  Hypersonic  
The Basis of an Industry-standard Aerodynamic Computation and its Theoretical Basis with Inferences and Applications 会议论文
7th Asian-Pacific Conference on Aerospace Technology and Science, 7th APCATS 2013, Taiwan, China, MAY 23-26, 2013
作者:  Gao Z(高智)
浏览  |  Adobe PDF(780Kb)  |  收藏  |  浏览/下载：536/150  |  提交时间：2014/03/11
Numerical Simulation  Hypersonic Flow  Viscous-inviscid Interacting Shear Flow (Isf)  Cfd Validation  Wall Momentum-energy Criteria