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Numerical Analysis and Dynamics of Large Deployable Membrane Structures

Numerical Analysis and Dynamics of Large Deployable Membrane Structures
大型可展开膜结构的数值分析和动力学
批准号:
21560826
负责人:
OKUIZUMI Nobukatsu
金额:
$2.91万
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2009
资助国家:
日本
项目状态:
已结题
起止时间:
2009 至 2011

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中文摘要
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英文摘要
In order to develop large membrane deployable structures, a multiple particle system model which is suited for efficient numerical analysis of membrane dynamics was developed and centrifugal deployment behaviors and vibration characteristics of membranes are studied. By inventing a model for crease stiffness and contact and adjusting the models for buckling and damping, it was confirmed that the numerical method could properly simulate small-scale centrifugal deployment experiments in vacuum. Vibration modes of a rotating circular membrane are also measured by creating an equipment which can rotate and shake a membrane simultaneously. The experimental results were compared with vibration mode analysis.
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Numerical Simulations of Centrifugal Deployments of Membranes by Spring-Mass System Models
通过弹簧质量系统模型对膜的离心展开进行数值模拟
DOI: --
发表时间: 2010
期刊:
影响因子: --
作者: [メザウィブラヒム, 庄司るり, 田丸人意, 樋口健,三輪武史,岩井達也,似鳥透,岩佐貴史,岸本直子, N. Okuizumi]
通讯作者: N. Okuizumi
らせん折り膜面の遠心力展開実験と数値シミュレーション
螺旋折叠膜表面的离心力发展实验和数值模拟
DOI: --
发表时间: 2009
期刊:
影响因子: --
作者: [樋口健, 三輪武史, 岩井達也, 似島透, 岩佐貴史, 岸本直子, 横井威, 奥泉信克]
通讯作者: 奥泉信克
DOI: --
发表时间: 2012
期刊: TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
影响因子: --
作者: [N.Okuizumi, A.Muta, S.Matsunaga]
通讯作者: S.Matsunaga
小型膜面構造モデルを用いた高真空スピン展開実験と解析
使用小型薄膜表面结构模型的高真空自旋膨胀实验与分析
DOI: --
发表时间: 2010
期刊:
影响因子: --
作者: [牟田梓, 松永三郎, 奥泉信克]
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