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Three-dimensional aeroacoustic numerical simulation of flow induced noise of mufflers 会议论文
26th International Conference on Parallel Computational Fluid Dynamics, ParCFD 2013, Changsha, China, May 20, 2013 - May 24, 2013
作者:  Yang Y(杨焱);  Sun HL;  Yang, Y. (yangy@ustc.edu)
浏览  |  Adobe PDF(1696Kb)  |  收藏  |  浏览/下载:245/94  |  提交时间:2017/05/27
Cfd (Computational Fluid Dynamics)  Computation Costs  Computational Aeroacoustics (Caa)  Design And Optimization  Flow Induced Noise  Non-linear Acoustics  Reynolds-averaged Navier-stokes  Three-dimensional Numerical Simulations  
Double-end-pumped Nd:YVO4 slab laser at 1064 nm 期刊论文
APPLIED OPTICS, 2012, 卷号: 51, 期号: 12, 页码: 2012-2014
作者:  Xu L;  Zhang HL;  He JL;  Yu XL(余西龙);  Cui L;  Mao YF;  Sun X;  Lin X;  Xing JC;  Xin JG;  Zhang, HL;  Beijing Inst Technol, Sch Optoelect, Beijing 100081, Peoples R China.
Adobe PDF(265Kb)  |  收藏  |  浏览/下载:694/180  |  提交时间:2013/01/18
Thin-disk Lasers  Nd:Yvo4 Slab  High-power  2nd-harmonic Generation  Efficient  Quality  
稀薄大气密度涨落对高空超高速飞行器气动性能的影响 会议论文
高超声速研讨会暨第五届全国高超声速科学技术会议, 中国广西桂林, 2012-11-12
作者:  蒋建政;  张羽淮;  李帅辉;  刘宏立;  孙泉华;  樊菁
浏览  |  Adobe PDF(62Kb)  |  收藏  |  浏览/下载:685/211  |  提交时间:2014/04/02
密度涨落  稀薄大气  高速飞行器  大气环境特性  太阳活动  气动性能  飞行器气动特性  热层  Dsmc  中间层  地磁效应  重力波  表面元  电离层  并行程序  下界  直接模拟  时空区域  高超声速  Stokes  
Development of a Cell Size Relaxed Scheme for the Direct Simulation Monte Carlo Method 会议论文
26th International Symposium on Rarefied Gas Dynmaics (RGD26), Kyoto, JAPAN, JUN 20-JUL 25, 2008
作者:  Sun QH(孙泉华);  Liu HL(刘宏立);  Fan J(樊菁);  Sun QH
Adobe PDF(460Kb)  |  收藏  |  浏览/下载:796/130  |  提交时间:2009/07/23
Direct Simulation Monte Carlo Method  Cell Size  Collision Scheme