Bird strike-induced damage studies on bio-inspired laminated plates with holes

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Aman Garg , Neeraj Kumar Shukla , Mohamed-Ouejdi Belarbi , Debasis Mukherjee , M. Pushpavalli , Roshan Raman , Mehmet Avcar , Mandeep Singh Narula , Li Li
{"title":"Bird strike-induced damage studies on bio-inspired laminated plates with holes","authors":"Aman Garg ,&nbsp;Neeraj Kumar Shukla ,&nbsp;Mohamed-Ouejdi Belarbi ,&nbsp;Debasis Mukherjee ,&nbsp;M. Pushpavalli ,&nbsp;Roshan Raman ,&nbsp;Mehmet Avcar ,&nbsp;Mandeep Singh Narula ,&nbsp;Li Li","doi":"10.1016/j.ast.2025.110200","DOIUrl":null,"url":null,"abstract":"<div><div>Bird strikes can potentially damage the aerospace and aeronautics structures and cause serious damage to the structure. In the present work, damage due to bird-strike in bio-inspired helicoidal laminated composite plates with circular and elliptical holes is predicted using Smoothed Particle Hydrodynamics (SPH)-Finite Element Method (FEM) model in ABAQUS. The Hashin failure model within ABAQUS has been implemented to model the impact-induced damage. The bird is modelled using the concepts of SPH to handle the mesh deformation problem effectively. Helicoidal recursive, exponential, semi-circular, linear, and Fibonacci helicoidal are studied during the present study. The plate is considered with two holes located at a quarter distance along the middle vertical axis of the plate. The damage in exponential, recursive, and linear helicoidal laminates is lesser than in conventional cross-ply and quasi-isotropic laminates. The plate with small dimensions of circular holes tends to deflect the failure in fibres towards the corners, while the plate with many holes arrests the cracks themselves. The plate with elliptical holes deflects the cracks towards themselves thus preventing the damage near the edges but damages the laminate in its vicinity.</div></div>","PeriodicalId":50955,"journal":{"name":"Aerospace Science and Technology","volume":"162 ","pages":"Article 110200"},"PeriodicalIF":5.0000,"publicationDate":"2025-04-05","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aerospace Science and Technology","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1270963825002718","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
引用次数: 0

Abstract

Bird strikes can potentially damage the aerospace and aeronautics structures and cause serious damage to the structure. In the present work, damage due to bird-strike in bio-inspired helicoidal laminated composite plates with circular and elliptical holes is predicted using Smoothed Particle Hydrodynamics (SPH)-Finite Element Method (FEM) model in ABAQUS. The Hashin failure model within ABAQUS has been implemented to model the impact-induced damage. The bird is modelled using the concepts of SPH to handle the mesh deformation problem effectively. Helicoidal recursive, exponential, semi-circular, linear, and Fibonacci helicoidal are studied during the present study. The plate is considered with two holes located at a quarter distance along the middle vertical axis of the plate. The damage in exponential, recursive, and linear helicoidal laminates is lesser than in conventional cross-ply and quasi-isotropic laminates. The plate with small dimensions of circular holes tends to deflect the failure in fibres towards the corners, while the plate with many holes arrests the cracks themselves. The plate with elliptical holes deflects the cracks towards themselves thus preventing the damage near the edges but damages the laminate in its vicinity.
带孔仿生层合板的鸟击损伤研究
鸟击有可能破坏航空航天结构,对结构造成严重损害。本研究利用 ABAQUS 中的平滑粒子流体力学(SPH)-有限元法(FEM)模型,预测了带圆孔和椭圆孔的生物启发螺旋形层压复合板因鸟击造成的损坏。ABAQUS 中的 Hashin 失效模型用于模拟冲击引起的损坏。该模型使用 SPH 概念有效处理网格变形问题。本研究对螺旋递归、指数、半圆、线性和斐波那契螺旋进行了研究。考虑到板上有两个孔,位于板中间垂直轴的四分之一处。与传统的交叉层压板和准各向同性层压板相比,指数、递归和线性螺旋形层压板的损伤较小。圆孔尺寸较小的层压板往往会将纤维的破坏偏向边角,而孔洞较多的层压板则会阻止裂缝的产生。带有椭圆孔的板可使裂缝向自身偏转,从而防止边缘附近的损坏,但会损坏其附近的层压板。
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 求助全文
来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
×
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
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
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 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信