Topology optimization of Nose Landing Gear of Aircraft for weight reduction

i) Zhang, Y., Chen, H., Chen, W., &Qian, L. (2020)Topology optimization design for landing gear brace structure under multi-
objective constraints.Structural and multidisciplinary optimization , 60(1), 267-283
ii) Zhang, L., Li, Y., Wang, J., & Yan, X. (2020). Structural topology optimization of landing gear upper fitting using particle swarm
optimization algorithm, Aerospace Science and Technology, 102, 105774
iii) Jia, X., Liu, Y., & Chen, J. (2020). Topology optimization design of aircraft landing gear beam based on ANSYS Workbench. Journal
of Physics: Conference Series, 1589(2), 022025.
iv) Li, H., Li, B., Li, Y., & Li, H. (2020). Topology optimization of the aircraft landing gear based on the stress criterion. Proceedings of
the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 234(9), 1667-1679.
v) Chen, X., & Wei, Y. (2020). Topology optimization design of aircraft landing gear with minimum weight and maximum stiffness.
International Journal of Aerospace Engineering, 2020.
vi) Zhang, C., Cheng, G., Liu, X., & Liu, J. (2020). Topology Optimization of landing gear based on geometric constraints,Journal of
Mechanical science and Technology,34(3),1073-1709.
vii) Nanda, A., & Das, D. (2020). Multi-objective topology optimization of an aircraft landing gear for minimum weight and maximum
stiffness using NSGA-II algorithm. Materials Today: Proceedings, 23, 1415-1422.
viii) Liu, J., Cheng, G., Liu, X., & Zhang, C. (2021). Topology optimization of aircraft landing gear based on manufacturing constraints.
Journal of Mechanical Science and Technology, 35(2), 793-799.
ix) Lin, L., & Li, Z. (2021). A novel multi-objective topology optimization method for aircraft landing gear structure design. Aerospace
Science and Technology, 112, 106679.