| Citation: | SHAO Haoyuan, LI Daochun, KAN Zi, et al. Rigid-flexible coupling dynamics simulation of carrier-based aircraft arrested landing under direct lift control[J]. Journal of Beijing University of Aeronautics and Astronautics. doi: 10.13700/j.bh.1001-5965.2024.0616(in Chinese)
|
Figures(1)
Copyright © Journal of Beijing University of Aeronautics and Astronautics
Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn
Supported by:
Beijing Renhe Information Technology Co., Ltd.
DownLoad: