In this work, an efficient topology optimization approach is proposed for a three-dimensional (3D) flexible multibody system (FMBS) undergoing both large overall motion and large deformation. The FMBS of concern is accurately modeled first via the solid element of the absolute nodal coordinate formulation (ANCF), which utilizes both nodal positions and nodal slopes as the generalized coordinates. Furthermore, the analytical formulae of the elastic force vector and the corresponding Jacobian are derived for efficient computation. To deal with the dynamics in the optimization process, the equivalent static load (ESL) method is employed to transform the topology optimization problem of dynamic response into a static one. Besides, the newly developed topology optimization method by moving morphable components (MMC) is used and reevaluated to optimize the 3D FMBS. In the MMC-based framework, a set of morphable structural components serves as the building blocks of optimization and hence greatly reduces the number of design variables. Therefore, the topology optimization approach has a potential to efficiently optimize an FMBS of large scale, especially in 3D cases. Two numerical examples are presented to validate the accuracy of the solid element of ANCF and the efficiency of the proposed optimization methodology, respectively.
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February 2018
Research-Article
Topology Optimization of a Three-Dimensional Flexible Multibody System Via Moving Morphable Components
Jialiang Sun,
Jialiang Sun
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China
e-mail: sunjialiang@nuaa.edu.cn
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China
e-mail: sunjialiang@nuaa.edu.cn
Search for other works by this author on:
Qiang Tian,
Qiang Tian
MOE Key Laboratory of Dynamics and Control of
Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: tianqiang_hust@aliyun.com
Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: tianqiang_hust@aliyun.com
Search for other works by this author on:
Haiyan Hu
Haiyan Hu
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China;
MOE Key Laboratory of Dynamics and Control
of Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: hhyae@nuaa.edu.cn
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China;
MOE Key Laboratory of Dynamics and Control
of Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: hhyae@nuaa.edu.cn
Search for other works by this author on:
Jialiang Sun
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China
e-mail: sunjialiang@nuaa.edu.cn
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China
e-mail: sunjialiang@nuaa.edu.cn
Qiang Tian
MOE Key Laboratory of Dynamics and Control of
Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: tianqiang_hust@aliyun.com
Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: tianqiang_hust@aliyun.com
Haiyan Hu
State Key Laboratory of Mechanics and Control
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China;
MOE Key Laboratory of Dynamics and Control
of Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: hhyae@nuaa.edu.cn
of Mechanical Structures,
College of Aerospace Engineering,
Nanjing University of Aeronautics and
Astronautics,
Nanjing 210016, China;
MOE Key Laboratory of Dynamics and Control
of Flight Vehicle,
School of Aerospace Engineering,
Beijing Institute of Technology,
Beijing 100081, China
e-mail: hhyae@nuaa.edu.cn
1Corresponding author.
Contributed by the Design Engineering Division of ASME for publication in the JOURNAL OF COMPUTATIONAL AND NONLINEAR DYNAMICS. Manuscript received July 26, 2017; final manuscript received September 23, 2017; published online November 9, 2017. Assoc. Editor: Zdravko Terze.
J. Comput. Nonlinear Dynam. Feb 2018, 13(2): 021010 (11 pages)
Published Online: November 9, 2017
Article history
Received:
July 26, 2017
Revised:
September 23, 2017
Citation
Sun, J., Tian, Q., and Hu, H. (November 9, 2017). "Topology Optimization of a Three-Dimensional Flexible Multibody System Via Moving Morphable Components." ASME. J. Comput. Nonlinear Dynam. February 2018; 13(2): 021010. https://doi.org/10.1115/1.4038142
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