タイトル | Better Finite-Element Analysis of Composite Shell Structures |
本文(外部サイト) | http://hdl.handle.net/2060/20090041661 |
著者(英) | Clarke, Gregory |
著者所属(英) | NASA Goddard Space Flight Center |
発行日 | 2007-05-01 |
言語 | eng |
内容記述 | A computer program implements a finite-element-based method of predicting the deformations of thin aerospace structures made of isotropic materials or anisotropic fiber-reinforced composite materials. The technique and corresponding software are applicable to thin shell structures in general and are particularly useful for analysis of thin beamlike members having open cross-sections (e.g. I-beams and C-channels) in which significant warping can occur. |
NASA分類 | Computer Programming and Software |
レポートNO | GSC-14756-1 |
権利 | Copyright, Distribution as joint owner in the copyright |