中文版 | English

在结果中检索

IMECH-IR

浏览/检索结果: 共18条，第1-10条 帮助

限定条件    
已选(0)清除 条数/页：   排序方式：
Investigation of high-order cell-centered finite difference method for aeroacoustics 会议论文
25th AIAA/CEAS Aeroacoustics Conference, 2019, Delft, Netherlands, May 20, 2019 - May 23, 2019
作者:  Jin Y;  Liao F(廖飞);  Cai JS;  Morris PJ
Adobe PDF(2986Kb)  |  收藏  |  浏览/下载：211/74  |  提交时间：2020/11/20
Development of zone flamelet model for scramjet combustor modeling 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);  Fan XJ(范学军)
浏览  |  Adobe PDF(623Kb)  |  收藏  |  浏览/下载：260/89  |  提交时间：2018/01/16
Combustion  Cost Benefit Analysis  Costs  Mixtures  Spacecraft  Supersonic Aircraft  
Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
作者:  Yao W(姚卫);  Fan XJ(范学军)
浏览  |  Adobe PDF(832Kb)  |  收藏  |  浏览/下载：274/81  |  提交时间：2018/11/08
Combustion  Cost benefit analysis  Costs  Mixtures  Ramjet engines  Supersonic aircraft  Computational costs  Equivalence ratios  Local flow conditions  Scramjet combustors  Statistics approaches  Supersonic combustion  Supersonic combustors  Turbulent combustion  
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  
Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
作者:  Gan JY;  Shen YQ(申义庆);  Zha GC
浏览  |  Adobe PDF(555Kb)  |  收藏  |  浏览/下载：279/91  |  提交时间：2017/05/05
Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
Non-oscillatory finite compact scheme for the equations of ideal magnetohydrodynamics 会议论文
International Symposium on Mechatronics and Applied Mechanics, ISMAM 2013, Nanjing, China, MAY 15-16, 2013
作者:  Liu L(刘利);  Shen YQ(申义庆);  Liu L(刘利)
浏览  |  Adobe PDF(487Kb)  |  收藏  |  浏览/下载：506/156  |  提交时间：2014/02/24
Shape design to minimize the peak heat-flux of blunt leading-edge 会议论文
51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2013, Grapevine, TX, United states, JAN 07-10, 2013
作者:  Cui K(崔凯);  Hu SC(胡守超);  Cui K(崔凯)
浏览  |  Adobe PDF(605Kb)  |  收藏  |  浏览/下载：628/306  |  提交时间：2014/02/24
Investigation of aerodynamic performance of high-speed train by detached eddy simulation 会议论文
1st International Workshop on High-Speed and Intercity Railways, IWHIR 2011, Shenzhen, Hong Kong, China, JULY 19-22, 2011
作者:  Zheng HW(郑洪伟);  Yang GW(杨国伟);  Zheng HW(郑洪伟)
Adobe PDF(778Kb)  |  收藏  |  浏览/下载：732/265  |  提交时间：2013/02/06
High Speed Train  Detached Eddy Simulation  Aerodynamic Performance  
Comparisons of high order hybrid schemes using a parameter-free discontinuity detector 会议论文
42nd AIAA Fluid Dynamics Conference and Exhibit 2012, New Orleans, LA, United states, JUN 25-28, 2012
作者:  Shen YQ(申义庆);  Zha GC;  Yang GW(杨国伟);  Gao Z(高智);  Shen YQ(申义庆)
浏览  |  Adobe PDF(2531Kb)  |  收藏  |  浏览/下载：480/106  |  提交时间：2014/02/24
基于混合网格NS 方程并行计算的某机全机颤振特性分析 会议论文
LHD2011夏季学术研讨会, 内蒙赤峰, 2011
作者:  郑冠男;  杨国伟;  钱卫
Adobe PDF(569Kb)  |  收藏  |  浏览/下载：418/138  |  提交时间：2014/01/23
Cfd  Csd  气动弹性  耦合算法  颤振特性  Mpi