个人简述:

1、 1999.12，飞机亚、超音速XXXX分析，航空工业总公司科学技术进步三奖（排名8）2、 2005.12，非线性XXXX分析技术与系统，国防科工委科学技术进步二等奖（排名6）3、 2007.12，XXXX试验测控、数据处理与可视化技术研究，航空工业总公司科学技术进步三奖（排名74、 2011.02，校园计算网格，陕西省科学技术奖三等奖（排名4）

科研工作:

1989-1990，重庆航天机电设计院助理工程师1999-2001，日本通产省工业技术院JST研究员1993- ，西北工业大学航空学院讲师（1995）、副教授（1998）、教授（2008） 科研项目：1、 高超声速下Lattice Boltzmann方法研究，航天科技创新基金，20092、 基于格子-Boltzmann方法的大涡湍流模拟，总装预研基金，20113、 全流域气体动理论方法研究，国家863项目，20114、 基于格子-Boltzmann方法的气动噪声研究，航空科学基金，20115、 基于格子Boltzmann方法的翼型层流转捩的大涡模拟研究，重点实验室基金，20136、 近空间高超声速飞行器层流转捩与湍流数值模拟方法研究，国家自然科学基金，20147、 XXX可压湍流数值研究，某预研基金重点项目，20148、基于气体动理学格式的等离子体流动控制机理数值研究，陕西省自然科学基础研究计划，2015  9、基于LES的边界层精细化数值模拟，某专项项目，2016 近期论文（2016至今)：1. Dongxin Pan, Chengwen Zhong, Congshan Zhuo. An Implicit Gas-Kinetic Scheme for Turbulent Flow on Unstructured Hybrid Mesh. Computers and Mathematics with Applications. (Accepted: 2018.02.11，中科院二区)2. Dongxin Pan, Chengwen Zhong, Congshan Zhuo. An Implicit Discrete Unified Gas-Kinetic Scheme for Simulations of Steady Flow in All Flow Regimes. Communications in Computational Physics. (Accepted: 2018.02.11，中科院二区)3. Ruifeng Yuan, Chengwen Zhong. An immersed-boundary method for compressible viscous flows and its application in the gas-kinetic BGK scheme. Applied Mathematical Modelling, 2018, 55: 417-446. (SCI: 000423005800026，中科院一区)4. Zhengxiong Hou, Chengwen Zhong, Christian Perez, Qing Zhang, Yunlan Wang. Experiences of Performance Optimization for Large Eddy Simulation on Intel MIC Platforms. In: Chen G., Shen H., Chen M. (eds) Parallel Architecture, Algorithm and Programming. PAAP 2017. Communications in Computer and Information Science, vol 729. Springer, Singapore. (EI: 20174204284602)5. 郭林亮，祝明红，傅澔，孔鹏，钟诚文. 一种低速风洞虚拟飞行试验装置的建模与仿真. 空气动力学学报，2017, 35(5): 708-717, 726.6. Yajun Zhu, Chengwen Zhong, Kun Xu. Unified Gas-kinetic Scheme with Multigrid Convergence for Rarefied Flow Study. Physics of Fluids, 2017, 29(9): 096102. (SCI: 000412105100046, EI: 20174004232277，中科院二区)7. Ji Li, Chengwen Zhong, Yong Wang, Congshan Zhuo. Implementation of dual time-stepping strategy of gas-kinetic scheme for unsteady flow simulations. Physical Review E, 95, 2017, 95(5): 053307. (SCI: 053307000402053500004, EI: 20172303741012，中科院二区).8. Linliang Guo, Minghong Zhu, Bowen Nie, Peng Kong, Chengwen Zhong. Initial virtual flight test for a dynamically similar aircraft model with control augmentation system. Chinese Journal of Aeronautics, 2017, 30(2): 602-610. (SCI: 000401138900013, EI: 20171203480980，中科院二区)9. Jieke Yao, Chengwen Zhong, Kebing Tang. An adaptive-gridding lattice Boltzmann method with linked-list data structure for two-dimensional viscous flows. Progress in Computational Fluid Dynamics, An International Journal, 2017, 17(5): 267-280. (SCI: 000411298000001, EI: 20173804187818，中科院四区)10. Ji Li, Chengwen Zhong, Dongxin Pan, Congshan Zhuo. A gas-kinetic scheme coupled with SST model for turbulent flows. Computers & Mathematics with Applications. (in press: 2016.09.30) (EI: 20164903100799，中科院二区)11. Congshan Zhuo, Chengwen Zhong. LES-based filter-matrix lattice Boltzmann model for simulating fully-developed turbulent channel flow. International Journal for Numerical Methods in Fluids, 2016, 30(7-10): 543-553. (SCI: 000388799800007, EI: 20164703025805，中科院三区)12. Dongxin Pan, Chengwen Zhong, Ji Li, Congshan Zhuo. A gas-kinetic scheme for the simulation of turbulent flows on unstructured meshes. International Journal for Numerical Methods in Fluids, 2016, 81(11): 748-769. (SCI: 000387206800003, EI: 20161902366254，中科院三区)13. Yajun Zhu, Chengwen Zhong, Kun Xu. Implicit Unified Gas-kinetic Scheme for Steady State Solution in All Flow Regimes. Journal of Computational Physics, 2016, 315: 16-38. (SCI: 000374832700002，中科院一区)14. 郭林亮，祝明红，孔鹏，聂博文，钟诚文. 风洞虚拟飞行模型机与原型机动力学特性分析. 航空学报，2016，37(8): 2583-2593. (EI: 20163602773123)15. Kai Li, Chengwen Zhong. Aeroacoustic simulations using compressible lattice Boltzmann method. Advances in Applied Mathematics and Mechanics, 2016, 8(5): 795-809. (SCI: 000379663500007，中科院四区)

教育背景:

1985-1989，南京航空学院空气动力学学系空气动力学专业  学士学位1990-1993，西北工业大学飞机系空气动力学专业  硕士学位1993-1997，西北工业大学飞机系空气动力学专业  博士学位