A reduced-order method for geometrically nonlinear analysis of the wing-upper-skin panels in the presence of buckling

Ke Liang, Zhen Yin, Qiuyang Hao. A reduced-order method for geometrically nonlinear analysis of the wing-upper-skin panels in the presence of buckling. Computers & Mathematics with Applications, 170:42-55, 2024. [doi]

@article{LiangYH24,
  title = {A reduced-order method for geometrically nonlinear analysis of the wing-upper-skin panels in the presence of buckling},
  author = {Ke Liang and Zhen Yin and Qiuyang Hao},
  year = {2024},
  doi = {10.1016/j.camwa.2024.06.014},
  url = {https://doi.org/10.1016/j.camwa.2024.06.014},
  researchr = {https://researchr.org/publication/LiangYH24},
  cites = {0},
  citedby = {0},
  journal = {Computers & Mathematics with Applications},
  volume = {170},
  pages = {42-55},
}