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Adaptive space transformation: An invariant based method for predicting aerodynamic coefficients of hypersonic vehicles 期刊论文
Engineering Applications of Artificial Intelligence, 2015, 卷号: 46, 页码: 93-103
作者:  Luo CT(罗长童);  Hu ZM(胡宗民);  Zhang SL;  Jiang ZL(姜宗林);  Luo, CT (reprint author), Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China.
浏览  |  Adobe PDF(1001Kb)  |  收藏  |  浏览/下载：337/118  |  提交时间：2016/01/07
Aerodynamic Coefficient  Data Correlation  Scaling Parameter  Genetic Programming  Invariant  
Relative contribution ratio: A quantitative metrics for multi-parameter analysis 期刊论文
Cogent Mathematics, 2015, 卷号: 2, 期号: 1, 页码: 1068979
作者:  Luo CT(罗长童);  Jiang ZL(姜宗林);  Wang C(王春);  Hu ZM(胡宗民)
浏览  |  Adobe PDF(1711Kb)  |  收藏  |  浏览/下载：280/74  |  提交时间：2016/01/07
On the numerical technique for the simulation of hypervelocity test flows 期刊论文
Computers & Fluids, 2015, 卷号: 106, 页码: 12-18
作者:  Hu ZM(胡宗民);  Wang C(王春);  Jiang ZL(姜宗林);  Khoo BC;  Hu ZM(胡宗民)
浏览  |  Adobe PDF(1617Kb)  |  收藏  |  浏览/下载：1577/919  |  提交时间：2014/11/27
Hypervelocity Test Flow  Dcd Scheme  Flux-splitting  Spurious Oscillation  
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel 会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
作者:  Wang YP(汪运鹏);  Hu ZM(胡宗民);  Liu YF(刘云峰);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(5104Kb)  |  收藏  |  浏览/下载：243/45  |  提交时间：2017/05/05
Inviscid Flows  Numerical Investigations  Outlet Diameters  Reflected Shock Waves  Simulated Results  Starting Process  Transmitted Shock  Unsteady Nozzle Flow  
A New Flux Splitting Scheme for Euler Equations of Gas Dynamics 会议论文
International Conference on Numerical Analysis and Applied Mathematics, Rhodes GREECE, SEP 22-28 2014
作者:  Li XD(李馨东);  Hu ZM(胡宗民);  Jiang ZL(姜宗林)
浏览  |  Adobe PDF(1140Kb)  |  收藏  |  浏览/下载：461/160  |  提交时间：2015/09/29
Flux Splitting  Hybrid Upwind Method  Ausm Scheme  K-cusp Scheme