研究方向
1、计算流体力学
2、空气动力学
3、气动弹性力学
教育/工作经历
1995-1999,西北工业大学空气动力学与飞行力学专业学士学位
1999-2001,西北工业大学大学流体力学专业硕士学位
2001-2005西北工业大学大学流体力学专业博士学位
2000-,西北工业大学航空学院讲师(2004)、副教授(2007)
代表著作
1.王刚,叶正寅,陈迎春.“三维非结构粘性网格生成方法”,计算物理,2001,Vol.18 No.5,402-406。
2.Wang gang, Ye Zhengyin. Mixed Element Type Unstructured Grid Generation and its Application to Viscous Flow Simulation, 24TH INTERNATIONAL CONGRESS OF AERONAUTICAL SCIENCES, 29 August - 3 September, 2004, Yokohama, Japan.
3.王刚,叶正寅。三维非结构混合网格生成与NS方程求解,航空学报, 2003, 24(5): 385-390.
4.Wang gang, Sun yingdan, Ye zhengyin. A Gridless Solution Method for Two-Dimensional Unsteady Flow. Chinese Journal of Aeronautics,Vol.18(1), pp: 8-14, 2005.
5.Wang Gang, Ye Zhengyin, Li Huaxing, Yang Qing. Studies on Aerodynamic Interferences between the Components of Transport Airplane using Unstructured Navier-Stokes Simulations. Computational Fluid Dynamics Journal, Vol.15 (1), pp: 191-197, 2006.
6.Li Chun-na, Ye Zheng-yin and Wang Gang. Simulation of the Flow Separation at the Wing-Body Junction with Different Fairings, Journal of Aircraft, 2008; 45(1): 258~266.
7.Wang Gang, Axel Schwoeppe, Ralf Heinrich. Comparison and Evaluation of Cell-centered and Cell-vertex Discretization in the Unstructured TAU Code for Turbulent Viscous Flows, 5th European Conference on Computational Fluid Dynamics, 14-17 June, 2010, Lisbon, Portugal.
8.王刚,许和勇,叶正寅。高阶间断有限元方法求解Euler方程时的数值积分问题研究,西北工业大学学报, Vol.29(1), pp:137-141, 2011.
9.Wang Gang, R. Heinrich, N. Kroll, Improved LU-SGS Relaxation Procedures in the TAU code According to the Coupling Way of Mean Flow and Turbulence Equations. 4th International conference on Computational Methods for Coupled Problems in Science and Engineering, 20-22 June 2011, Kos, Greece.
10.Wang Gang,Jiang Yuewen,Ye Zhengyin. An Improved LU-SGS Implicit Scheme for High Reynolds Number Flow Computations on Hybrid Unstructured Mesh, Chinese Journal of Aeronautics,Vol.25(1), 2012.
科研概况
1、局部流动分离诱导的结构振动问题研究,国家自然基金,2009-2011
讲授课程
1、流体力学基础(I),本科生课程,64学时
获奖情况
1、2006.12,基于非结构网格的复杂流场分析技术及系统,省科技进步三等奖(排名2)
2、2009.12,高效高精度气动弹性分析系统,国防科学技术进步奖(三等奖),(排名7)