@inproceedings{b02ff72d5bf34b30ba53a066fe1f0100,
title = "Topology optimization for eigenvalue problems in aerospace structure design with rigid links",
abstract = "The main purpose of this paper is to present an aerospace engineering application of topology optimization for maximizing eigenvalue problem. In this problem, the internal structure of a rocket which is supposed to support four satellites needs to be designed. To improve the vibration performance of the whole structure, the topology optimization technology is introduced to gain a suitable structure configuration. To simplify the model, satellites are regarded as lumped masses and connecting to their supporting structure with rigid links.",
keywords = "Aerospace structure design, Eigenvalue, Rigid links, Topology optimization",
author = "Zhu, {Ji Hong} and Gao, {Huan Huan} and Jie Hou",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.483.510",
language = "英语",
isbn = "9783037859834",
series = "Applied Mechanics and Materials",
pages = "510--513",
booktitle = "Mechanical Engineering, Materials and Energy III",
note = "2013 3rd International Conference on Mechanical Engineering, Materials and Energy, ICMEME 2013 ; Conference date: 09-11-2013 Through 10-11-2013",
}