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| Parametric study on wing-lambda-shock formation 会议论文
Fluids Engineering Division Summer Meeting, FEDSM 2021, Virtual, Online, 10 August 2021 到 12 August 2021
作者: Chainok S; Rungroch T; Chairach P; Prapamonthon P; Yooyen S; Yin B(银波) ; Yang GW(杨国伟); Ju SJ(鞠胜军)
 Adobe PDF(3026Kb) |  收藏 | 浏览/下载：270/86 | 提交时间：2021/11/30
Shock Supersonic flow Transonic flow |
| Direct Numerical Simulation of Hypersonic Boundary-layer Transition of Blunt cones 会议论文
Tenth International Conference on Computational Fluid Dynamics (ICCFD10), Barcelona, Spain, Jule 9-13, 2018
作者: Li XL(李新亮); Yu ZP(于长平); Tong FL(童福林)
Adobe PDF(2711Kb) | 收藏 | 浏览/下载：333/55 | 提交时间：2018/12/05 |
| NUMERICAL ANALYSIS ON DRAG REDUCTION OF HIGH-SPEED TRAIN USING ROUGH SURFACE 会议论文
ASME Fluids Engineering Division Summer Meeting (FEDSM2018), Montreal, CANADA, JUL 15-20, 2018
作者: Yin B(银波); Yang GW(杨国伟)
Adobe PDF(1595Kb) | 收藏 | 浏览/下载：208/43 | 提交时间：2019/04/19 |
| A comparative study of elliptical and round scramjet combustors by Improved Delayed Detached Eddy Simulation 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Fan XJ(范学军); Fan, Xuejun(xfan@imech.ac.cn)
Adobe PDF(1173Kb) | 收藏 | 浏览/下载：435/214 | 提交时间：2018/01/16
Adiabatic Flame Temperature Aerodynamics Boundary Layer Flow Boundary Layers Chemical Analysis Combustion Computational Chemistry Directed Graphs Flow Separation Mach Number Principal Component Analysis Regression Analysis Sensitivity Analysis Spacecraft Supersonic Aerodynamics Supersonic Aircraft Transients |
| Experimental Studies of Film Cooling in Supersonic Combustors 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Fan C(樊川); Wang J(王晶); Fan XJ(范学军)
Adobe PDF(735Kb) | 收藏 | 浏览/下载：305/99 | 提交时间：2018/01/16
Combustion Combustors Coolants Kerosene Spacecraft Supersonic Aerodynamics |
| Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp 会议论文
Meeting of the Institute-of-Non-Newtonian-Fluid-Mechanics (INNFM), Llanwddyn, WALES, 2017
作者: Tong FL(童福林); Li XL(李新亮); Duan, Yanhui; Yu ZP(于长平); Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
Adobe PDF(3818Kb) | 收藏 | 浏览/下载：294/117 | 提交时间：2018/01/16
Concave Surface Curvature Adverse Pressure-gradient Large-eddy Simulation Reynolds-number Near-wall Flows Separation Vortices Models |
| Normal acceleration reduce guidanceand control for sub-orbit vehicle re-entry 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Li WH(李文皓); Xiao XX(肖歆昕); Zhang H(张珩); Xiao XX(肖歆昕)
Adobe PDF(1066Kb) | 收藏 | 浏览/下载：411/89 | 提交时间：2018/01/16
Aerodynamics Air Navigation Angle Of Attack Control Surfaces Control Theory Degrees Of Freedom (Mechanics) Dynamic Models Flight Control Systems Flight Simulators Monte Carlo Methods Reentry Spacecraft Surface Reactions Uncertainty Analysis Vehicles |
| Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Li GL(李广利); Cui K(崔凯); Xiao Y(肖尧); Xu YZ(徐应洲)
Adobe PDF(664Kb) | 收藏 | 浏览/下载：377/89 | 提交时间：2018/01/16
Aerodynamics Angle Of Attack Angle Of Attack Indicators Boundary Layers Drag Drag Coefficient High Pressure Effects Hypersonic Aerodynamics Hypersonic Flow Spacecraft |
| Study on Compression Surface Deformation of Waveriders 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Xu YZ(徐应洲); Cui K(崔凯); Li GL(李广利); Xiao Y(肖尧)
Adobe PDF(461Kb) | 收藏 | 浏览/下载：303/83 | 提交时间：2018/01/16
Aerodynamic Configurations Aerodynamics Computational Fluid Dynamics Deformation Evolutionary Algorithms Fluid Dynamics Hypersonic Aerodynamics Optimization Spacecraft |
| Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Wang Q(汪球); Li JW; Lu P; Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林)
Adobe PDF(679Kb) | 收藏 | 浏览/下载：382/67 | 提交时间：2018/01/16
Calibration Detonation Heat Transfer Nozzles Spacecraft Supersonic Aerodynamics Thermodynamics Uncertainty Analysis |
