龚春林科研成果

个人经历 Personal experience 工作经历 教育经历 1.2004.4至今，西北工业大学航天学院，教师 2.2014.1~2015.1，德国宇航院（DLR）流体与空气动力学研究所，访问学者 西北工业大学，本科，1997~2001 西北工业大学，硕士，2001~2004 西北工业大学，博士，2003~2007

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教育教学

教育教学 Education and teaching 教育教学 1、本科生课程(1)《航天飞行器设计》（56学时）(2)《飞行器系统工程》（32学时）(3)《导弹总体设计原理》（国家精品课程）（40学时）(4)《航天概论》（8学时）2、研究生课程(1)《空天飞行器总体设计》（40学时）(2)《Multidisciplinary Design Optimization Methodology for Flight Vehicle》（40学时）(3)《飞行器总体设计实践》（20学时） 内容来自集群智慧云企服 发明专利4999元代写全部资料全国受理

荣誉获奖

科学研究 Scientific Research (1) 导弹和先进空天飞行器总体设计(2) 飞行器多学科设计优化(3) 武器系统仿真与效能评估

科学研究

学术成果 Academic Achievements 1. 期刊论文（英文）2021年(1) Gao G., Gou J.-J., Gong C. L.*, Hu J.-X., Gao R.-C.. A novel mechanical-thermal-electrical thermal protection system concept and its multi-scale performance evaluation for hypersonic launch vehicles, Composite Structures, 2021, 268: 113962(2) Fang H., Gong C. L. *, Li C. N., Zhang Y. W., Ronch A. D..   A sequential optimization framework for simultaneous design variables optimization and probability uncertainty allocation, Structural and Multidisciplinary Optimization,2021,63(3): 1307-1325(3) Zhang Y. W., Gong C. L. *, Li C. N.. Efficient time-variant reliability analysis through approximating the most probable point trajectory, Structural and Multidisciplinary Optimization , 2021, 63(1): 289-309(4) Gou J.-J., Yan Z.-W., Hu J.-X., Gao G., Gong C. L. *. The heat dissipation, transport and reuse management for hypersonic vehicles based on regenerative cooling and thermoelectric conversion, Aerospace Science and Technology, 2021, 108: 1063732020年(1) Li C.-N., Fang H., Gong C. L. *.  Development of an efficient global optimization method based on adaptive infilling for structure optimization，Structural and Multidisciplinary Optimization, 2020,62(6): 3383-3412(2) Chen X. Y., Li C. N., Gong C. L. *, Gu L. X., Ronch A. D..  A study of morphing aircraft on morphing rules along trajectory, Chinese Journal of Aeronautics, 20202019年(1)   Fang Z., Gong C. L. *, Revell  A., Chen  G., Harwood A., O'Connor J.. Passive separation control of a NACA0012 airfoil via a flexible flap. Physics of Fluids, 2019, 31(10)(2)   Gou J.-J., Chang Y., Yan Z.-W., Chen B., Gong C. L. *. The design of thermal management system for hypersonic launch vehicles based on active cooling networks, Applied Thermal Engineering. 2019, 159: 1139382018年之前(1) Zhang Y. W., Gong C. L.*, Fang H., Ronch D. A. An efficient space division–based width optimization method for RBF network using fuzzy clustering algorithms. STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, https://doi.org/10.1007/s00158-019-02217-7.(2) Fang H., Gong C. L.*, Su H., Zhang Y.W., Li C. N., Li X., Ronch A. D.. A gradient based uncertainty optimization framework utilizing dimensional adaptive polynomial chaos expansion. STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, Doi: http://doi.org/10.1007/s00158-018-2123-z.(3) Gong C. L., Han J. K., Yuan Z. J., Fang Z., Chen G. Numerical investigation of the effects of different parameters on the thrust performance of three dimensional flapping wings. AEROSPACE SCIENCE AND TECHNOLOGY, Vol84(2019):431-445.(4) Li X., Gong C. L.*, Gu L. X., Zhao J., Fang H., Gao R. C.. A Reliability-based Optimization Method Using Sequential Surrogate Model and Monte Carlo Simulation, STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, Vol59(2):439-460, 2019.02.(5) Fang H., Gong C. L.*, Li C. N., Li X., Su H., Gu L. X.. A Surrogate Model Based Nested Optimization Framework for Inverse Problem Considering Interval Uncertainty. STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION, Vol58(3):869-883, 2018.10.(6) Gong C. L., Fang Z., Chen G. A Lattice Boltzmann-Immersed Boundary-Finite Element Method for nonlinear fluid–solid interaction simulation with moving objects. INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, Vol15(7):1850063:1-27, 2018.10.(7) Gou J. J., Gong C. L., Gu L. X., et al. The unit cell method in predictions of thermal expansion properties of textile reinforced composites. COMPOSITE STRUCTURES, Vol195(2018): 99-117, 2018.07.(8) Gong C. L., Gou J. J., Hu J. X., et al. A novel TE-material based thermal protection structure and its performance evaluation for hypersonic flight vehicles. AEROSPACE SCIENCE AND TECHNOLOGY, Vol77(2018):458-470, 2018.06.(9) Gong C. L., Shi Z., Zhang Y., et al. Fabrication and thermoelectric properties of Ca-Co-O ceramics with negative Seebeck coefficient. RESULTS IN PHYSICS, Vol9(2018): 1233-1238, 2018.06.(10) Gong C. L., Fang Z., Chen G., et al. Numerical investigation of nonlinear fluid–structure interaction dynamic behaviors under a general Immersed Boundary-Lattice Boltzmann-Finite Element method. INTERNATIONAL JOURNAL OF MODERN PHYSICS C, Vol29(4):1850038, 2018.05.(11) Gong C. L., Yuan Z. J., Zhou Q., etal. Numerical investigation of unsteady flows past flapping wings with Immersed Boundary-Lattice Boltzmann method. JOURNAL OF MECHANICS, Vol34(2): 193-207, 2018.04.(12) Gong C. L., Wang Y., Gu L.X., et al. An approach for stress analysis of corrugated-core integrated thermal protection system under thermal and mechanical environment. COMPOSITE STRUCTURES, Vol185(2018): 1-26, 2018.02.(13) Li C. N., Wei Q., Gong C. L, et al. An efficient multiple point selection study for mesh deformation using radial basis functions. AEROSPACE SCIENCE AND TECHNOLOGY, Vol71(2017): 580-591, 2017.12.(14) Gou J. J., Gong C. L., Gu L. X., et al. Unit cells of composites with symmetric structures for the study of effective thermal properties. APPLIED THERMAL ENGINEERING, Vol126(2017): 602-619, 2017.11.(15) Gong C. L., Dong G., Hu J.X., et al. Effect of reducing annealing on the microstructure and thermoelectric properties of La-Bi co-doped SrTiO3 ceramics. JOURNAL OF MATERIALS SCIENCE-MATERIALS IN ELECTRONICS, Vol28(19): 14893-14900, 2017.10.(16) Su H., Gong C. L., Gu L. X. Three-Dimensional CST Parameterization Method Applied in Aircraft Aeroelastic Analysis. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, Vol2017(1874729 ): 1-15, 2017.04.(17) Su H., Gong C. L., Gu L. X. Kernel Parameter Optimization for Kriging Based on Structural Risk Minimization Principle. MATHEMATICAL PROBLEMS IN ENGINEERING, Vol2017(3021950 ): 1-9, 2017.04.(18) Gong C. L., Gu L.X.. A novel SMOTE-based classification approach to online data imbalance problem. MATHEMATICAL PROBLEMS IN ENGINEERING, Vol2016(5685970):1-14, 2016.04.(19) Sun X. F., Gu L. X., Gong C. L. Dynamics of a deflectable-nose missile. SCIENCE CHINA-TECHNOLOGICAL SCIENCES, Vol55 (12): 3483-3494, 2012.12.  2、期刊论文（中文）2021年(1) 胡嘉欣，芮姝，高瑞朝，苟建军，龚春林. 飞行器结构布局与尺寸混合优化方法研究, 航空学报, V.20210429.1135.028.html.(2) 缪佶,龚春林,李春娜. 基于CFD收敛提前终止和变复杂度模型的两级气动优化方法,   西北工业大学学报, 2021, 39(01): 148-158.2020年(1) 杨泗智,龚春林,郝波,吴蔚楠,谷良贤. 基于落点预测的高旋火箭弹弹道修正算法, 航空学报, 2020, 41(02): 303-311.(2) 陈兵, 仇理宽, 龚春林, 谷良贤. 流-固-推进耦合下的机体/推进一体化性能分析, 推进技术, 2020, 41(04): 729-739.2019年(1) 唐硕, 龚春林, 陈兵. 组合动力空天飞行器关键技术, 宇航学报, 2019, 40(10): 1103-1114.2018年之前(1)  龚春林，赤丰华，谷良贤，方海. 基于Karhunen-Loève展开的分布式变体飞行器最优控制方法，航空学报，2018，(2): 83-96(2) 龚春林，朱政光，陈兵，粟华，谷良贤. 多段分支弹道的两级全局优化方法，宇航学报，2017 , 38 (9): 903-910(3) 龚春林，韩璐，谷良贤. 适应于RBCC运载器的轨迹优化建模研究，宇航学报，2013 , 34 (12) :1592-1598(4) 龚春林，韩璐. RBCC可重复使用运载器上升段轨迹优化设计，固体火箭技术，2012, Vol35（3）：290-295.(5) 龚春林，谷良贤，粟华. 亚轨道重复使用运载器总体多学科优化方法, 固体火箭技术, 2012, 35(1): 5-10(6) 龚春林，谷良贤，孙建勋. 基于多学科设计优化技术的导弹方案设计，计算机集成制造系统，2009, 15(5)：842-847(7) 龚春林，谷良贤，袁建平. 面向飞行器多学科设计优化的主模型技术，宇航学报，2009, 30(3)：914-918(8) 龚春林，谷良贤，袁建平. 基于全局优化算法的多学科优化计算构架，西北工业大学学报，2009, 27(1)：52-56(9) 龚春林，顾振芳，赵吉松. 基于整体级概念的多级固体运载火箭设计与优化，固体火箭技术，2009, 32(1)：1-5(10) 龚春林，谷良贤. 高超声速飞行器多学科优化建模方法，计算机集成制造系统，2008, 14(9)：1690-1695(11) 龚春林，谷良贤，袁建平. 基响应面的变复杂度气动分析模型，西北工业大学学报，2006, 24(4)：532-535(12) 龚春林，袁建平，谷良贤. 基统分解的多学科集成设计过程与工具，计算机集成制造系统，2006, 12(3)：334-338 3、国际会议论文(1) Chun-Lin Gong, Bing Chen, Liang-Xian Gu, Shuo Tang. The airframe/propulsion integrated design, analysis and ground test for RBCC launch vehicle，AIAA-2017-2318, 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March, 2017(2) Chun-Lin Gong, Bing Chen, Liang-Xian Gu. Comparison Study of RBCC Powered Suborbital Reusable Launch Vehicle Concepts, AIAA-2015-3606, 20th AIAA International Space and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July, 2015(3) Chun-Lin Gong, Bing Chen, Liang-Xian Gu. Design and Optimization of RBCC powered suborbital reusable launch vehicle, AIAA-2014-2361, 19th AIAA International Space and Hypersonic Systems and Technologies Conference，Atlanta，GA，USA，16-20 June, 2014(4) Chun-Lin Gong, Liang-Xian Gu. Multidisciplinary Design & Optimization Models and Software Tool for Hypersonic Flight Vehicle, IAC09.C4.5.9, 60th International Astronautic Congress, Daejeon, South Korea, 12-16 Oct., 2009(5) Chun-Lin Gong, Liang-Xian Gu, Jian-Ping Yuan, Li Wang. A Rapid Aerodynamics/Propulsion Analysis Method for Hypersonic Flight Vehicle MDO. AIAA-2006-7994. 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference, Canberra, Australia, 6-9 Nov., 2006 4、授权发明专利(1) 一种变结构二维超音速进气道调节装置，国家发明专利ZL201610504772.8，2018.10.26，排名第1.(2) 一种宽速域变结构尾喷管的调节装置，国家发明专利ZL201610710381.1，2018.10.02，排名第1.(3) 一种吸气式超燃冲压发动机的推力架结构，国家发明专利ZL201610710112.5，2018.08.21，排名第1.(4) 一种变结构二维进气道调节装置，国家发明专利ZL201610502968.3，2018.04.13，排名第1.(5) 一种对称型变结构超音速进气道调节装置，国家发明专利ZL201610503099.6，2017.11.28，排名第1.(6) 一种封闭式变结构二维超音速进气道，国家发明专利ZL201610504745.0 ，2017.10.31，排名第1.(7) 面向多层次性能的导弹总体多学科优化方法，国家发明专利ZL201410404496.9 ，2017.02.08，排名第1.(8) 折叠式手机卫星结构，国家发明专利ZL201410209563.1，2016.06.08，排名第1.(9) 一种实现巡飞器翼身连接、固定、锁死、解锁的一体化结构，国家发明专利ZL201410292609.0，2016.03.30，排名第1.(10) 具有自搭载发射功能的新型纳卫星结构，国家发明专利ZL201310210744.1， 2016.02.17，排名第1. 内容来自集群智慧云企服 www.jiqunzhihui.net

学术成果

荣誉获奖 Awards Information (1)  入选教育部万名双创导师人才库，2017(2)  飞行器多学科设计与优化平台. 国防科技进步三等奖，第1名，2015(3)  运载器虚拟仿真技术. 军委科技进步二等奖，第6名，2012 (4)  多学科设计优化技术体系与框架软件. 陕西省科学技术三等奖，第2名，2010(5)  多方位打造精品，构建航天创新型人才培养体系. 陕西省普通高校教学成果二等奖，第3名，2012 内容来自集群智慧云企服

综合介绍

社会兼职 Social Appointments (1) 中国兵工学会导弹与火箭第七届专业委员会委员(2) 《系统工程与电子技术》第九届编委会委员 内容来自集群智慧云企服 软件著作权666元代写全部资料全国受理