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| Numerical and Experimental Study on Vertical Takeoff and Separation of the Compound Aircraft 期刊论文
IEEE ACCESS, 2022, 卷号: 10, 页码: 47597-47617
作者: Wang D; Hong QZ(洪启臻) ; Huang X(黄鑫); Pei XB; Wang J
 Adobe PDF(4750Kb) |  收藏 | 浏览/下载：154/23 | 提交时间：2022/07/18
Aircraft Aircraft propulsion Compounds Aerodynamics Engines Automotive components Tail Compound aircraft CFD vertical take-off dynamical separation of two aircraft |
| Longitudinal aerodynamic modeling and verification for air-launch-to-orbit system during stage separation 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 21
作者: Yang L(杨磊); Ye, Zhengyin; Li WH(李文皓); Sun QH(孙泉华)
Adobe PDF(4621Kb) | 收藏 | 浏览/下载：253/51 | 提交时间：2021/11/01
Store separation Aerodynamic modeling Interference aerodynamics Dynamic simulation Air-launch-to-orbit |
| Local Piston Theory with Viscous Correction and Its Application 期刊论文
AIAA Journal, 2017, 卷号: 55, 期号: 3, 页码: 942-954
作者: Liu W(刘文); Zhang CA(张陈安); Han HQ; Wang FM(王发民); Zhang, CA (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
 浏览 | Adobe PDF(1329Kb) | 收藏 | 浏览/下载：572/114 | 提交时间：2017/03/28
Hypersonic Unsteady Aerodynamics Piston Theory Aeroelasticity |
| 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)
浏览 | Adobe PDF(1173Kb) | 收藏 | 浏览/下载：440/216 | 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)
浏览 | Adobe PDF(735Kb) | 收藏 | 浏览/下载：308/101 | 提交时间：2018/01/16
Combustion Combustors Coolants Kerosene Spacecraft Supersonic Aerodynamics |
| 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)
浏览 | Adobe PDF(664Kb) | 收藏 | 浏览/下载：382/91 | 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 |
| Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者: Xiao Y(肖尧); Cui K(崔凯); Li GL(李广利); Xu YZ(徐应洲)
浏览 | Adobe PDF(639Kb) | 收藏 | 浏览/下载：277/88 | 提交时间：2018/01/16
Aerodynamics Air Engines Aspect Ratio Computational Fluid Dynamics Drag Engines Hypersonic Aerodynamics Lift Lift Drag Ratio Propulsion Spacecraft Vehicles |
| 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)
浏览 | Adobe PDF(461Kb) | 收藏 | 浏览/下载：305/84 | 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)
浏览 | Adobe PDF(679Kb) | 收藏 | 浏览/下载：386/68 | 提交时间：2018/01/16
Calibration Detonation Heat Transfer Nozzles Spacecraft Supersonic Aerodynamics Thermodynamics Uncertainty Analysis |
| Performance of a 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: Li JW; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX
浏览 | Adobe PDF(468Kb) | 收藏 | 浏览/下载：295/82 | 提交时间：2018/01/16
Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |
