Simulation methodology for high velocity impact in composite aircraft structures

Alastair Johnson
{"title":"Simulation methodology for high velocity impact in composite aircraft structures","authors":"Alastair Johnson","doi":"10.1016/S1290-0958(01)90057-7","DOIUrl":null,"url":null,"abstract":"<div><p>The paper summarises the IMT Project HICAS on ‘High Velocity Impact of Composite Aircraft Structures’ which was concerned with developing a design methodology and FE simulation tools for predicting the high velocity impact response of composite aircraft structures. Achievements include measurement of high rate mechanical properties of three aircraft composite systems, development of new failure models for composites under high rate loads, implementation of models into commercial FE codes and code validation by simulation of impact in test structures.</p></div>","PeriodicalId":100069,"journal":{"name":"Air & Space Europe","volume":"3 3","pages":"Pages 56-59"},"PeriodicalIF":0.0000,"publicationDate":"2001-05-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1290-0958(01)90057-7","citationCount":"4","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Air & Space Europe","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1290095801900577","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 4

Abstract

The paper summarises the IMT Project HICAS on ‘High Velocity Impact of Composite Aircraft Structures’ which was concerned with developing a design methodology and FE simulation tools for predicting the high velocity impact response of composite aircraft structures. Achievements include measurement of high rate mechanical properties of three aircraft composite systems, development of new failure models for composites under high rate loads, implementation of models into commercial FE codes and code validation by simulation of impact in test structures.

查看原文
分享 分享
微信好友 朋友圈 QQ好友 复制链接
本刊更多论文
复合材料飞机结构高速碰撞仿真方法
本文总结了IMT项目HICAS“复合材料飞机结构的高速冲击”,该项目涉及开发一种设计方法和有限元模拟工具,用于预测复合材料飞机结构的高速冲击响应。取得的成就包括测量三种飞机复合材料系统的高速率力学性能,开发新的复合材料在高速率载荷下的失效模型,将模型应用于商业有限元代码中,并通过在测试结构中模拟冲击来验证代码。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 去求助
来源期刊
自引率
0.00%
发文量
0
期刊最新文献
Foreword The End…or…the End of a Benginning? Firms & Institutions CEAS Public Policy
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
现在去查看 取消
×
提示
确定
0
微信
客服QQ
Book学术公众号 扫码关注我们
反馈
×
意见反馈
请填写您的意见或建议
请填写您的手机或邮箱
已复制链接
已复制链接
快去分享给好友吧!
我知道了
×
扫码分享
扫码分享
Book学术官方微信
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术
文献互助 智能选刊 最新文献 互助须知 联系我们:info@booksci.cn
Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。
Copyright © 2023 Book学术 All rights reserved.
ghs 京公网安备 11010802042870号 京ICP备2023020795号-1