日本航空宇宙学会誌
Online ISSN : 2424-1369
Print ISSN : 0021-4663
ISSN-L : 0021-4663
直交異方性材料積層板の四点曲げ試験法
(II) 実験
加藤 譲古賀 達蔵
著者情報
ジャーナル フリー

1990 年 38 巻 442 号 p. 608-615

詳細
抄録

This paper presents four-point bending tests to examine pure bending deformation of rectangular symmetric crossplies of fiber reinforced composites. The bending deformation is visualized and measured by holographic interferometry. Test results show that the pure bending deformation is realized, at least in a central portion of a specimen, provided that the aspect ratios of the specimen between the supporting and the loading points fall into certain ranges depending on the laminate composition. The higher the ratio of the axial to the transverse bending rigidity is, the greater the aspect ratios are required. These confirm the theoretical predictions made by a numerical analysis in a preceding paper of the authors'. Specific values of the aspect ratios are recommended for various laminate compositions.

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