学术论文 [1]A 4-node thin shell element based on co-rotational for laminated composite structures. International Journal of Numerical Methods for Calculation and Design in Engineering (SCI4区). 第一作者. 2018,34(1). [2]Nonlinear aeroelastic characteristics analysis of composite wing with high aspect ratio based on co-rotational method. Journal of Fluids and Structures(SCI 2区).第一作者. 2018(82). [3]Effect of Stiffness on Flutter of Composite Wings with High Aspect Ratio. Mathematical Problems in Engineering(SCI 4区). 第一作者. 2021(2021). [4]The impact and sensitivity analysis of beam and stringer for stiffness center of composite wing structure. Revista Internacional de Métodos Numéricos para Cálculo y Diseño en Ingeniería(SCI 4区).第一作者. 2021(37). [5]Static Aeroelastic Analysis of Composite Wings with a Large Aspect Ratio Based on the CFD/CSD Method. Journal of Aeronautics, Astronautics and Aviation(EI(期刊)). 第一作者. 2021(53). [6]A Numerical Study of the Impact of Bending and Torsional Stiffness on the Static Aeroelastic Characteristics of a Large Aspect Ratio CompositeWing, International Journal of Numerical Methods for Calculation and Design in Engineering (SCI4区). 第一作者. 2025,41(2). |