Evaluation of Compressive Nonlinear Response of Unidirectional Carbon Fiber Reinforced Composites using a Modified Sandwich Beam Specimen in Flexure

Author:

Yokozeki Tomohiro1,Ogasawara Toshio2,Ishikawa Takashi3

Affiliation:

1. Department of Aeronautics and Astronautics, University of Tokyo, 7-3-1 Hongo Bunkyo-ku, Tokyo 113-8656, Japan, -tokyo.ac.jp

2. Advanced Composite Technology Center, Institute of Aerospace Technology (IAT), Japan Aerospace Exploration Agency (JAXA), 6-13-1 Osawa, Mitaka Tokyo 181-0015, Japan

3. Aviation Program Group (APG), Japan Aerospace Exploration Agency (JAXA) 7-44-1 Jindaiji Higashi-machi, Chofu, Tokyo 182-8522, Japan

Abstract

Nonlinear mechanical behaviors of unidirectional composites were evaluated under compressive loading up to high-strain ranges using a sandwich beam specimen with the emphasis on the elastic material nonlinearity in the fiber direction. Specimen configuration and evaluation method, including material nonlinear effects, were proposed, and the compressive nonlinear behavior and strength of unidirectional carbon fiber reinforced composites were experimentally obtained. The measured compressive behaviors were compared with those from coupon-type compression tests of unidirectional and quasi-isotropic laminates. The compressive strength of unidirectional laminates evaluated, using the present sandwich method, was much higher than that of coupon specimens, whereas the failure strain of the former was almost identical to that of coupon-type quasi-isotropic laminates. The proposed method is expected to contribute to the accurate evaluation technology of compression behaviors of unidirectional laminates up to high-strain ranges.

Publisher

SAGE Publications

Subject

Materials Chemistry,Polymers and Plastics,Mechanical Engineering,Mechanics of Materials,Ceramics and Composites

Reference20 articles.

1. ASTM-D 3410. (2004). Annual Book of ASTM Standards, Vol. 15.03, ASTM International, West Conshohocken.

2. A comparison of test techniques used for the evaluation of the unidirectional compressive strength of carbon fibre-reinforced plastic

Cited by 8 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3