王晓喆 - 北京航空航天大学

个人简介

教育背景 2013.9~2019.3：北京航空航天大学航空科学与工程学院，博士 2018.1~2019.1：英国利兹大学机械工程学院，CSC公派 2009.9~2013.6：北京航空航天大学高等工程学院，学士 2006.9~2009.6：东北师范大学附属中学，高中工作经历 2019.7~至今：北京航空航天大学无人系统研究院，讲师所获奖励中国科协青年人才托举工程, 国家级青年人才项目, 2022 中国航空学会科学技术奖, 二等奖, 排名2/8, 2020 北京市教育教学成果奖, 二等奖, 排名7/10, 2021 科研项目主持国防重点实验室基金、航天科学技术基金、民航开放研究基金、航空航天研究院所课题等项目；作为主要完成人深度参与了民机专项科研、重点研发计划、十三五装备预研、基础加强计划、自然科学基金等项目。项目研究内容涉及无人机总体方案设计、无人机防撞技术、气动弹性分析、气动弹性优化等多个领域

研究领域

飞行器设计气动弹性优化飞行载荷分析无人机总体设计

近期论文

查看导师最新文章（温馨提示：请注意重名现象，建议点开原文通过作者单位确认）

Wang, Xiaozhe; Zhang, S.S.; Wan, Z.Q.*; Wang, Z. Aeroelastic Topology Optimization of Wing Structure Based on Moving Boundary Meshfree Method. Symmetry-Basel, 2022, 14(6): 1154. (SCI检索) Wang, Z.; Wan, Z.; Groh, R.; Wang, Xiaozhe*. Aeroelastic and local buckling optimisation of a variable-angle-tow composite wing-box structure. Composite Structures, 2021, 258: 113201. (SCI检索) Liu, Y.; Wan, Z.; Yang, C.; Wang, Xiaozhe*. NURBS-Enhanced Meshfree Method with an Integration Subtraction Technique for Complex Topology. Applied Sciences-Basel, 2020, 10(7): 2587. (SCI检索) Dong, G; Wang, Xiaozhe*; Liu, D*. Metaheuristic Approaches to Solve a Complex Aircraft Performance Optimization Problem. Applied Sciences-Basel, 2019, 9(15): 2979. (SCI检索) Wang, Xiaozhe; Wan, Z.; Liu, Z.; Yang, C*. Integrated optimization on aerodynamics-structure coupling and flight stability of a large airplane in preliminary design. Chinese Journal of Aeronautics, 2018, 31(6): 1258-1272. (SCI检索) Wan, Z.; Wang, Xiaozhe; Yang, C*. Integrated aerodynamics/structure/stability optimization of large aircraft in conceptual design. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2018, 232(4): 745-756. (SCI检索) Wan, Z.; Wang, Xiaozhe; Yang, C*. A Highly Efficient Aeroelastic Optimization Method Based on a Surrogate Model. International Journal of Aeronautical and Space Sciences, 2016, 17(4): 491-500. (SCI检索) Wang, Xiaozhe; Qin, C.; Li, K.Y.; Wan, Z.Q.; Liu, Q.H. Integrated Aerostructural Optimization and Flight Stability Analysis throughout Design Process of Large Aircraft. APISAT 2022. (EI检索) Li, W.X.; Wan, Z.Q.; Wang, Xiaozhe*; Yang, C. FNO-thermal Surrogate Model for Rapid Aerothermoelastic Analysis of Hypersonic Wing. APISAT 2022. (EI检索) Wang, Z.; Ma, J.X.; Wang, Xiaozhe*; Xu, G.H.; Chen, G.P. Uncertain resource allocation in UAV from the perspective of distributed robust games. AICS 2022. (EI检索) Li, C.; Wan, Z.; Wang, Xiaozhe*. An Integrated Aerodynamic/Thermal/Structural Design Framework for Hypersonic Vehicles. ICAS 2020/2021. (EI检索) Zhang, S.; Wan, Z.; Wang, Xiaozhe*. Topology Optimization for Wing Structure of Hypersonic Vehicle. ICAS 2020/2021. (EI检索) 李旭阳; 万志强; 王晓喆*; 杨璐嘉; 杨超. 考虑多巡航工况的大型飞机气动弹性优化. 北京航空航天大学学报, 2021, 47(8): 1628-1637. (EI检索) Wang, Xiaozhe*; Wan, Z.; Yang, C. Research on Applicability of Integrated Design Optimization in Blended Wing Body Aircraft. AIAA Scitech 2019 Forum. (EI检索) Wang, Xiaozhe*; Wan, Z.; Yang, C. An integrated optimization and surrogate analysis of large aircraft in conceptual design. IFASD 2017. (EI检索) Wang, Xiaozhe*; Wan, Z.; Yang, C. A High-efficiency Aeroelastic Optimization Method Based on Kriging Model and Genetic Algorithm. IFASD 2015. (EI检索) 王晓喆*; 万志强; 杨超; 刘耘臻. 面向飞机各设计阶段考虑静气动弹性效应的面元法飞行载荷分析方法, 气体物理, 2020, 5(6): 16-25. (核心检索)