中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共4条，第1-4条 帮助

限定条件    
已选(0)清除 条数/页：   排序方式：
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：438/216  |  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  
LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
作者:  Wu K(吴坤);  Zhang P(张鹏);  Yao W(姚卫);  Fan XJ(范学军);  Zhang, Peng(pengzhang.zhang@polyu.edu.hk)
浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载：298/89  |  提交时间：2018/01/16
Combustion  Diesel Engines  Hydrogen  Large Eddy Simulation  Spacecraft  Stabilization  Supersonic Aircraft  Temperature Measurement  Wall Flow  
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)
浏览  |  Adobe PDF(1066Kb)  |  收藏  |  浏览/下载：413/89  |  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  
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