Computer Center, National Aerospace Laboratory(NAL)
出版者
航空宇宙技術研究所
出版者（英）
National Aerospace Laboratory(NAL)
雑誌名
航空宇宙技術研究所報告
雑誌名(英)
Technical Report of National Aerospace Laboratory TR-850
巻
850
ページ
11
発行年
1985-01
抄録（英）
Stress eigenstates at the loaded end in symmetric laminated plates are discussed in this paper. The rate of attenuation of nonuniform stress distribution in composite materials is slow in comparison with that in isotropic materials. For a graphite/epoxy cross-ply laminate, for example, the characteristic length le is approximately three times that for an isotropic material. It is emphasized that the evaluation by numerical method of this decay is important in estimating the strength of composite laminated plates.
対称積層板における端末効果の数値解析
naltr00850.pdf
(677.69KB)
