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3点曲げ試験による積層CFRPの面外方向引張弾性率
https://jaxa.repo.nii.ac.jp/records/22493
https://jaxa.repo.nii.ac.jp/records/2249326b648b2-36c0-4c55-afb5-a65240c133f5
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 3点曲げ試験による積層CFRPの面外方向引張弾性率 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Out-of-plane | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mechanical properties | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Test method | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Bending test | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Out-of-Plane Tensile Modulus of CFRP Laminates by 3-Point Bending Test | |||||
著者 |
原, 栄一
× 原, 栄一× 横関, 智弘× 八田, 博志× 岩堀, 豊× 石川, 隆司× Hara, Eiichi× Yokozeki, Tomohiro× Hatta, Hiroshi× Iwahori, Yutaka× Ishikawa, Takashi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部(JAXA) | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構航空本部(JAXA) | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
出版者 | ||||||
出版者 | 日本複合材料学会 | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Composite Materials | |||||
書誌情報 |
日本複合材料学会誌 en : Journal of the Japan Society for Composite Materials 巻 39, 号 5, p. 184-192, 発行日 2013-09-15 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | To propose a test method for the out-of plane tensile modulus of laminated carbon fiber-reinforced plastics, 3-point bending tests using a laminated CGRP with the span direction coinciding with out-of-plane (through-the-thickness) direction were performed. It was demonstrated that the apparent bending modulus depends on the length of span to thickness ratio (L/t) and the tensile modulus E to shear modulus G ratio (E/G). Sensitivity analyses were performed to select the length of span to thickness ratio in order to evaluate the bending modulus near material modulus. Consequently, it is predicted that the bending modulus performed with the L/t >25 bending specimen is equivalent to tensile modulus, if the apparent bending modulus were evaluated from 1 to 15GPa, while modified equations for the out-of-plane modulus of QI-CFRP laminates obtained by three-dimensional laminate theory were also derived. This modification took stress condition in consideration of the small in-plane size like bending specimens into account. Moreover, it is demonstrated that apparent bending moduli were evaluated between upper and lower-bound solutions. The upper-bound solution is an out-of-plane modulus based on existing three-dimensional laminate theory, and the other is modified out-of-plane modulus. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0385-2563 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN00196748 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.6089/jscm.39.184 | |||||
関連名称 | info:doi/10.6089/jscm.39.184 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1420046000 |