[1]     Wang X.Z., Xia K.J., Wu K., Wan Z.Q*. A Surrogate Model of Composite Mechanics Based on Data/Physics Hybrid Driven Method[C]. ICAUS 2024.

[2]     王晓喆, 王钰博, 吴坤, 万志强*. 面向垂直轴风力发电机的柔性叶片结构优化[J]. 北京航空航天大学学报, 2024, 10.13700/j.bh.1001-5965.2024.0444.

[3]     Zhang S.S., Wan Z.Q., Wang X.Z.*, Xu A., Chen Z.Y. Analysis of Flight Loads during Symmetric Aircraft Maneuvers Based on the Gradient-Enhanced Kriging Model[J]. Aerospace, 2024, 11(5): 334.

[4]     Sun Z., Wan Z.Q., Wang X.Z.*, Ma L., Li C. Aerothermoelasticity Analysis of Hypersonic Vehicle Based on Meshfree Method[C]. IFASD 2024.

[5]     Ma L., Wan Z.Q., Wang X.Z.*, Li K.Y., He L.F. A CFD/CSD Based Aero-Thermo-Elastic Framework for Full-Vehicle Scale Analysis[C]. IFASD 2024.

[6]     Li K.Y., Yang C., Wang X.Z.*, Wan Z.Q., Ma L., Li C. Aeroelastic Optimization of Large Aircraft Considering High-Precision Aerodynamic Performance[C]. IFASD 2024.

[7]     Li C., Wan Z.Q., Wang X.Z.*, Yang C., Li K.Y. Semianalytical Research on Aerothermoelastic Behaviors of Functionally Graded Plates under Arbitrary Temperature Fields in Hypersonic Vehicles[J]. Aerospace, 2024, 11: 572.

[8]     Li C., Wan Z.Q., Wang X.Z.*, Yang C., Chen Z.Y. An Integrated Static/Dynamic Aerothermoelastic Analysis Framework for Functionally Graded Structures in Hypersonic Vehicles[C]. IFASD 2024.

[9]     万志强, 张珊珊, 王晓喆*, 马靓, 许翱, 吴志刚, 杨超. 弹性飞机飞行载荷分析及减缓技术综述[J]. 航空学报, 2024, 10.7527/S1000-6893.2024.30279.

[10]   李畅, 万志强, 王晓喆*, 杨超, 黎珂宇. 热载荷环境下金属-陶瓷功能梯度板的屈曲特性研究[J]. 北京航空航天大学学报, 2024, 10.13700/j.bh.1001-5965.2023.0658.

[11]   黎珂宇, 杨超, 王晓喆*, 万志强, 李畅. 基于多种微结构的机翼结构/材料气动弹性优化[J]. 北京航空航天大学学报, 2024, 10.13700/j.bh.1001-5965.2024.0178.

[12]   Li K.Y., Yang C., Wang X.Z.*, Wan Z.Q., Li C. Multiscale Aeroelastic Optimization Method for Wing Structure and Material[J]. Aerospace, 2023, 10(10): 866.

[13]   王泽溪, 万志强, 王晓喆*, 杨超. 曲线纤维壁板屈曲/后屈曲建模与快速分析方法[J]. 北京航空航天大学学报, 2023, 49(2): 353-366.

[14]   李旭阳, 万志强, 王晓喆*. 面向联结翼总体设计的气动弹性优化[J]. 北京航空航天大学学报, 2023, 49(12): 3343-3354.

[15]   黄胤铮, 王晓喆*, 王柳青. 基于伴随理论的无人机气动弹性优化[J]. 软件导刊, 2023, 22(10): 26-32.

[16]   Wang Z., Ma J.X., Wang X.Z.*, Xu G.H., Chen G.P. Uncertain resource allocation in UAV from the perspective of distributed robust games[C]. 4th International Conference on Artificial Intelligence and Computer Science, AICS 2022.

[17]   Wang X.Z., Zhang S.S., Wan Z.Q.*, Wang Z. Aeroelastic Topology Optimization of Wing Structure Based on Moving Boundary Meshfree Method[J]. Symmetry, 2022, 14(6): 1154.

[18]   Wang X.Z., Qin C., Li K.Y., Wan Z.Q.*, Liu Q.H. Integrated Aerostructural Optimization and Flight Stability Analysis throughout Design Process of Large Aircraft[C]. APISAT 2022.

[19]   Li W.X., Wan Z.Q., Wang X.Z.*, Yang C. FNO-thermal Surrogate Model for Rapid Aerothermoelastic Analysis of Hypersonic Wing[C]. APISAT 2022.

[20]   Zhang S.S., Wan Z.Q., Wang X.Z.*, Liu Y.Z. Topology Optimization for Wing Structure of Hypersonic Vehicle[C]. ICAS 2020/2021.

[21]   Wang Z.X., Wan Z.Q., Groh R.M.J., Wang X.Z*. Aeroelastic and local buckling optimisation of a variable-angle-tow composite wing-box structure[J]. Composite Structures, 2021, 258: 113201.

[22]   Li X.Y., Wan Z.Q., Wang X.Z.*, Yang C. Aeroelastic Optimization Design of the Global Stiffness for a Joined Wing Aircraft[J]. Applied Sciences, 2021, 11(24): 11800.

[23]   Li C., Wan Z.Q., Wang X.Z*. An Integrated Aerodynamic/Thermal/Structural Design Framework for Hypersonic Vehicles[C]. ICAS 2020/2021.

[24]   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[J]. 北京航空航天大学学报, 2021, 47(8): 1628-1637.

[25]   Liu Y.Z., Wan Z.Q.*, Yang C., Wang X.Z. NURBS-Enhanced Meshfree Method with an Integration Subtraction Technique for Complex Topology[J]. Applied Sciences, 2020, 10(7): 2587.

[26]   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[J]. 气体物理, 2020, 5(6): 16-25.

[27]   Wang X.Z., Wan Z.Q., Yang C*. Research on Applicability of Integrated Design Optimization in Blended Wing Body Aircraft[C]. AIAA Scitech 2019 Forum.

[28]   Dong G.R., Wang X.Z.*, Liu D.Z. Metaheuristic Approaches to Solve a Complex Aircraft Performance Optimization Problem[J]. Applied Sciences, 2019, 9(15): 2979, 10.3390/app9152979.

[29]   Wang X.Z., Wan Z.Q., Liu Z., Yang C*. Integrated optimization on aerodynamics-structure coupling and flight stability of a large airplane in preliminary design[J]. Chinese Journal of Aeronautics, 2018, 31(6): 1258-1272.

[30]   Wan Z.Q., Wang X.Z., Yang C*. Integrated aerodynamics/structure/stability optimization of large aircraft in conceptual design[J]. Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering, 2018, 232(4): 745-756.

[31]   Wang X.Z., Wan Z.Q., Yang C*. An integrated optimization and surrogate analysis of large aircraft in conceptual design[C]. IFASD 2017.

[32]   Wan Z.Q., Wang X.Z., Yang C*. A Highly Efficient Aeroelastic Optimization Method Based on a Surrogate Model[J]. International Journal of Aeronautical and Space Sciences, 2016, 17(4): 491-500.

[33]   Wang X.Z., Wan Z.Q., Yang C*. A high-efficiency aeroelastic optimization method based on kriging model and genetic algorithm[C]. IFASD 2015.