日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
対称積層材の剛性特性とその設計法
福永 久雄関根 英樹
著者情報
ジャーナル フリー

42 巻 (1994) 485 号 p. 371-380

詳細
PDFをダウンロード (4542K) 発行機関連絡先
抄録

Symmetric laminates exhibit extension-shear or bending-twisting coupling. In a stiffness design of laminates, it is important to make use of coupling terms. The present paper clarifies stiffness characteristics of symmetric laminates using the lamination parameters. The feasible regions of the lamination parameters are examined for several conventional symmetric laminates and stiffness characteristics are represented on the lamination parameter plane. The feasibility and limitation of a stiffness design are discussed for conventional laminates. Based on the fundamental relation of the lamination parameters, a method is developed for determining laminate configurations corresponding to the in-plane or out-of-plane lamination parameters. A genetic algorithm is also applied to the determination of laminate configurations in a stiffness design of laminates.

著者関連情報
© The Japan Society for Aeronautical and Space Sciences
前の記事 次の記事

閲覧履歴
feedback
Top