TY - JOUR
T1 - Topology optimization of joint load control with geometrical nonlinearity
AU - HOU, Jie
AU - GU, Xiaojun
AU - ZHU, Jihong
AU - WANG, Jie
AU - ZHANG, Weihong
N1 - Publisher Copyright:
© 2019 Chinese Society of Aeronautics and Astronautics
PY - 2020/1
Y1 - 2020/1
N2 - This paper presents an extended topology optimization approach considering joint load constraints with geo-metrical nonlinearity in design of assembled structures. The geometrical nonlinearity is firstly included to reflect the structural response and the joint load distribution under large deformation. To avoid a failure of fastener joints, topology optimization is then carried out to minimize the structural end compliance in the equilibrium state while controlling joint loads intensities over fasteners. During nonlinear analysis and optimization, a novel implementation of adjoint vector sensitivity analysis along with super element condensation is introduced to address numerical instability issues. The degrees of freedom of weak regions are condensed so that their influences are excluded from the iterative Newton-Raphson (NR) solution. Numerical examples are presented to validate the efficiency and robustness of the proposed method. The effects of joint load constraints and geometrical nonlinearity are highlighted by comparing numerical optimization results.
AB - This paper presents an extended topology optimization approach considering joint load constraints with geo-metrical nonlinearity in design of assembled structures. The geometrical nonlinearity is firstly included to reflect the structural response and the joint load distribution under large deformation. To avoid a failure of fastener joints, topology optimization is then carried out to minimize the structural end compliance in the equilibrium state while controlling joint loads intensities over fasteners. During nonlinear analysis and optimization, a novel implementation of adjoint vector sensitivity analysis along with super element condensation is introduced to address numerical instability issues. The degrees of freedom of weak regions are condensed so that their influences are excluded from the iterative Newton-Raphson (NR) solution. Numerical examples are presented to validate the efficiency and robustness of the proposed method. The effects of joint load constraints and geometrical nonlinearity are highlighted by comparing numerical optimization results.
KW - Geometrical nonlinearity
KW - Joint load constraint
KW - Sensitivity analysis
KW - Super element condensation
KW - Topology optimization
UR - http://www.scopus.com/inward/record.url?scp=85062271066&partnerID=8YFLogxK
U2 - 10.1016/j.cja.2019.01.024
DO - 10.1016/j.cja.2019.01.024
M3 - 文章
AN - SCOPUS:85062271066
SN - 1000-9361
VL - 33
SP - 372
EP - 382
JO - Chinese Journal of Aeronautics
JF - Chinese Journal of Aeronautics
IS - 1
ER -