Modeling of gossamer space structures with distributed transfer function method

被引:2
|
作者
Fang, HF
Lou, M
Yang, BG
Yang, YB
机构
[1] CALTECH, Jet Prop Lab, Mech Syst Engn & Res Div, Pasadena, CA 91109 USA
[2] Univ So Calif, Dept Aerosp & Mech Engn, Los Angeles, CA 90089 USA
关键词
D O I
10.2514/2.3976
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A new structural modeling and analysis method, the distributed transfer function method, is presented for application to gossamer space structures. The distributed transfer function method uses distributed transfer functions, instead of shape function used by traditional finite element solvers, to represent the displacement field. The distributed transfer function method maintains the modeling flexibility of the finite element method, so that it is capable of modeling multibody, complex structures, but it requires much fewer nodes and results in a significant reduction of computational time. The distributed transfer functions give rise to closed-form analytical solutions of both displacement and strain fields. As a result, the distributed transfer function method only decomposes a structure at those points where multiple components are connected, to keep each component as large as possible. Gossamer space structures are generally composed of several long booms and large membranes.. Therefore, the distributed transfer function method can be used to model a gossamer structure with a small number of unknowns and matrices of low order. It offers very accurate results with high computational efficiency. The distributed transfer function method is applied to investigate the sensitivity of buckling strength of an inflatable/rigidizable boom to the variations in bending stiffness.
引用
收藏
页码:548 / 552
页数:5
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