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  1. B200 工学部/工学研究科
  2. B200a 雑誌掲載論文
  3. 学術雑誌

High fidelity simulation of low velocity impact behavior of CFRP laminate

http://hdl.handle.net/2237/00029251
http://hdl.handle.net/2237/00029251
eb7b1b41-ceb0-44ba-997b-53c6fda84053
名前 / ファイル ライセンス アクション
Final-Composites_A_Revised.pdf Final-Composites_A_Revised (4.1 MB)
Item type 学術雑誌論文 / Journal Article(1)
公開日 2019-02-06
タイトル
タイトル High fidelity simulation of low velocity impact behavior of CFRP laminate
言語 en
著者 Ebina, Masaya

× Ebina, Masaya

WEKO 88614

en Ebina, Masaya

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Yoshimura, Akinori

× Yoshimura, Akinori

WEKO 88615

en Yoshimura, Akinori

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Sakaue, Kenichi

× Sakaue, Kenichi

WEKO 88616

en Sakaue, Kenichi

Search repository
Waas, Anthony M.

× Waas, Anthony M.

WEKO 88617

en Waas, Anthony M.

Search repository
アクセス権
アクセス権 open access
アクセス権URI http://purl.org/coar/access_right/c_abf2
権利
言語 en
権利情報 © 2018. This manuscript version is made available under the CC-BY-NC-ND 4.0 license http://creativecommons.org/licenses/by-nc-nd/4.0/
キーワード
主題Scheme Other
主題 Impact behavior
キーワード
主題Scheme Other
主題 Transverse cracking
キーワード
主題Scheme Other
主題 Finite element analysis (FEA)
キーワード
主題Scheme Other
主題 Damage mechanics
抄録
内容記述 In this paper, a finite element (FE) model which simulates damage extent of CFRP laminate subjected to low velocity face-on impact is proposed. The validity of the model is demonstrated by comparing experimental and numerical results for two different CFRPs with different stacking sequence and boundary conditions. Experimental damage extent were obtained from the drop-weight test and non-destructive inspections (C-scan, radiograph and X-ray CT). Numerical results were obtained from FE analyses done on Abaqus/Explicit 2016. In the present model, each damage mode is modeled separately. Fiber damage is modeled by smeared crack model (SCM). In-plane ply cracks are modeled by the enhanced continuum damage mechanics (ECDM) model, which is composed of continuum damage mechanics (CDM) and SCM. Delamination between laminae is modeled by cohesive behavior based on the contact formulation. For both CFRPs, numerical results obtained from the present model show reasonable agreement with experimental results.
言語 en
内容記述タイプ Abstract
内容記述
内容記述 ファイル公開:2020-10-01
言語 ja
内容記述タイプ Other
出版者
言語 en
出版者 Elsevier
言語
言語 eng
資源タイプ
資源タイプresource http://purl.org/coar/resource_type/c_6501
タイプ journal article
出版タイプ
出版タイプ AM
出版タイプResource http://purl.org/coar/version/c_ab4af688f83e57aa
DOI
関連タイプ isVersionOf
識別子タイプ DOI
関連識別子 https://doi.org/10.1016/j.compositesa.2018.07.022
ISSN(print)
収録物識別子タイプ PISSN
収録物識別子 1359-835X
書誌情報 en : Composites Part A: Applied Science and Manufacturing

巻 113, p. 166-179, 発行日 2018-10
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