Correlation of CFRP and AA7075 Aircraft Wing box structure using FEM

Abstract Composite materials are becoming more important in the construction of Mechanical structures. The primary objective of this paper is to analyse the Carbon Fibre Reinforced Plastic (CFRP) and Aluminium alloy (AA 7075) aircraft wing box using finite element method. Both results has been corre...

Full description

Saved in:
Bibliographic Details
Published inIOP conference series. Materials Science and Engineering Vol. 1126; no. 1; p. 12081
Main Authors Vigneshwaran, M., Kumaran, M, Praveen, kumar K, Revanth, K, Sathya, prakash T
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.03.2021
Subjects
Aircraft
Aluminum base alloys
Carbon fiber reinforced plastics
Composite materials
Finite element method
Mathematical models
Weight reduction
Wing boxes
Wings (aircraft)
Online AccessGet full text

Cover

Abstract Abstract Composite materials are becoming more important in the construction of Mechanical structures. The primary objective of this paper is to analyse the Carbon Fibre Reinforced Plastic (CFRP) and Aluminium alloy (AA 7075) aircraft wing box using finite element method. Both results has been correlated. Both CFRP and AA7075 structures modelling and numerical simulations were executed at various loading conditions. The deformed configuration of the CFRP and AA7075 aircraft wing box along with stress plot have been computed using analysis. Based on these studies, the CFRP and AA7075 central wing box, representing a weight saving of up to one and a half tonnes compared to the most advanced aluminium alloys. The results also expose the increasing strength with reduced weight.
AbstractList Composite materials are becoming more important in the construction of Mechanical structures. The primary objective of this paper is to analyse the Carbon Fibre Reinforced Plastic (CFRP) and Aluminium alloy (AA 7075) aircraft wing box using finite element method. Both results has been correlated. Both CFRP and AA7075 structures modelling and numerical simulations were executed at various loading conditions. The deformed configuration of the CFRP and AA7075 aircraft wing box along with stress plot have been computed using analysis. Based on these studies, the CFRP and AA7075 central wing box, representing a weight saving of up to one and a half tonnes compared to the most advanced aluminium alloys. The results also expose the increasing strength with reduced weight.
Abstract Composite materials are becoming more important in the construction of Mechanical structures. The primary objective of this paper is to analyse the Carbon Fibre Reinforced Plastic (CFRP) and Aluminium alloy (AA 7075) aircraft wing box using finite element method. Both results has been correlated. Both CFRP and AA7075 structures modelling and numerical simulations were executed at various loading conditions. The deformed configuration of the CFRP and AA7075 aircraft wing box along with stress plot have been computed using analysis. Based on these studies, the CFRP and AA7075 central wing box, representing a weight saving of up to one and a half tonnes compared to the most advanced aluminium alloys. The results also expose the increasing strength with reduced weight.
Author Kumaran, M
Vigneshwaran, M.
Praveen, kumar K
Sathya, prakash T
Revanth, K
Author_xml – sequence: 1
  givenname: M.
  surname: Vigneshwaran
  fullname: Vigneshwaran, M.
– sequence: 2
  givenname: M
  surname: Kumaran
  fullname: Kumaran, M
– sequence: 3
  givenname: kumar K
  surname: Praveen
  fullname: Praveen, kumar K
– sequence: 4
  givenname: K
  surname: Revanth
  fullname: Revanth, K
– sequence: 5
  givenname: prakash T
  surname: Sathya
  fullname: Sathya, prakash T
BookMark eNo9kFFLwzAUhYNMcJv-BgM-1-YmTZM-lrpNYaKIom8hTRPpmM1MWtB_b8tkT-dy7uEc-BZo1vnOInQN5BaIlCkILhJZFB8pAM1TSAlQIuEMzU-f2emWcIEWMe4IyUWWkTm6q3wIdq_71nfYO1ytX56x7hpcloIIjss2mKBdj9_b7hPX_gfHPgymH4LFQ5y89erxEp07vY_26l-X6G29eq3uk-3T5qEqt4kByiGRtAHL83GXOc1MwS1nojFWGHBUZw6ohkzqJhNWWp1rTutMs1pYmjeOyYIt0c2x9xD892Bjr3Z-CN04qcZ-KPKCSj6mxDFlgo8xWKcOof3S4VcBURMyNcFQExg1IVOgjsjYHyfmXo0
Cites_doi 10.1016/j.surfcoat.2013.10.049
10.1016/S0955-2219(00)00047-9
10.1155/2013/671469
10.1016/j.ast.2011.04.008
ContentType Journal Article
Copyright 2021. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
Copyright_xml – notice: 2021. This work is published under http://creativecommons.org/licenses/by/3.0/ (the “License”). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License.
DBID AAYXX
CITATION
8FE
8FG
ABJCF
ABUWG
AFKRA
AZQEC
BENPR
BGLVJ
CCPQU
D1I
DWQXO
HCIFZ
KB.
L6V
M7S
PDBOC
PIMPY
PQEST
PQQKQ
PQUKI
PRINS
PTHSS
DOI 10.1088/1757-899X/1126/1/012081
DatabaseName CrossRef
ProQuest SciTech Collection
ProQuest Technology Collection
Materials Science & Engineering Collection
ProQuest Central (Alumni)
ProQuest Central
ProQuest Central Essentials
ProQuest Central
Technology Collection
ProQuest One Community College
ProQuest Materials Science Collection
ProQuest Central Korea
SciTech Premium Collection
Materials Science Database
ProQuest Engineering Collection
Engineering Database
Materials Science Collection
Publicly Available Content Database
ProQuest One Academic Eastern Edition (DO NOT USE)
ProQuest One Academic
ProQuest One Academic UKI Edition
ProQuest Central China
Engineering Collection
DatabaseTitle CrossRef
Publicly Available Content Database
ProQuest Materials Science Collection
Engineering Database
Technology Collection
ProQuest Central Essentials
ProQuest One Academic Eastern Edition
Materials Science Collection
ProQuest Central (Alumni Edition)
SciTech Premium Collection
ProQuest One Community College
ProQuest Technology Collection
ProQuest SciTech Collection
ProQuest Central China
ProQuest Central
ProQuest Engineering Collection
ProQuest One Academic UKI Edition
ProQuest Central Korea
Materials Science & Engineering Collection
Materials Science Database
ProQuest One Academic
Engineering Collection
DatabaseTitleList Publicly Available Content Database
CrossRef
Database_xml – sequence: 1
  dbid: 8FG
  name: ProQuest Technology Collection
  url: https://search.proquest.com/technologycollection1
  sourceTypes: Aggregation Database
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
EISSN 1757-899X
ExternalDocumentID 10_1088_1757_899X_1126_1_012081
Genre Conference Proceeding
GroupedDBID 1JI
5B3
5PX
5VS
AAJIO
AAJKP
AAYXX
ABHWH
ABJCF
ACAFW
ACGFO
ACHIP
ACIPV
AEFHF
AEJGL
AFKRA
AFYNE
AHSEE
AIYBF
AKPSB
ALMA_UNASSIGNED_HOLDINGS
ASPBG
ATQHT
AVWKF
AZFZN
BENPR
BGLVJ
CCPQU
CEBXE
CITATION
CJUJL
CRLBU
EBS
EDWGO
EQZZN
GROUPED_DOAJ
GX1
HCIFZ
HH5
IJHAN
IOP
IZVLO
KB.
KNG
KQ8
M7S
N5L
O3W
OK1
P2P
PDBOC
PIMPY
PJBAE
PTHSS
RIN
RNS
SY9
T37
TR2
W28
8FE
8FG
ABUWG
AZQEC
D1I
DWQXO
L6V
PQEST
PQQKQ
PQUKI
PRINS
ID FETCH-LOGICAL-c1251-82d1e564403fa3c95e537dce7c1f2a4f12a148ad47e8ea6a52b4a3b7e26df3893
IEDL.DBID 8FG
ISSN 1757-8981
IngestDate Thu Oct 10 17:23:21 EDT 2024
Fri Aug 23 00:41:12 EDT 2024
IsDoiOpenAccess true
IsOpenAccess true
IsPeerReviewed true
IsScholarly true
Issue 1
Language English
LinkModel DirectLink
MergedId FETCHMERGED-LOGICAL-c1251-82d1e564403fa3c95e537dce7c1f2a4f12a148ad47e8ea6a52b4a3b7e26df3893
OpenAccessLink https://www.proquest.com/docview/2511969285?pq-origsite=%requestingapplication%
PQID 2511969285
PQPubID 4998670
ParticipantIDs proquest_journals_2511969285
crossref_primary_10_1088_1757_899X_1126_1_012081
PublicationCentury 2000
PublicationDate 2021-03-01
20210301
PublicationDateYYYYMMDD 2021-03-01
PublicationDate_xml – month: 03
  year: 2021
  text: 2021-03-01
  day: 01
PublicationDecade 2020
PublicationPlace Bristol
PublicationPlace_xml – name: Bristol
PublicationTitle IOP conference series. Materials Science and Engineering
PublicationYear 2021
Publisher IOP Publishing
Publisher_xml – name: IOP Publishing
References Immanuvel (MSE_1126_1_012081bib3) 2014
Gruber (MSE_1126_1_012081bib4) 2013; 12
Arunachalam (MSE_1126_1_012081bib6) 2013
Han (MSE_1126_1_012081bib11) 2013; 236
Mrazova (MSE_1126_1_012081bib1) 2013; 5
Kang (MSE_1126_1_012081bib2)
Rathnakar (MSE_1126_1_012081bib5) 2013; 2
Chiang (MSE_1126_1_012081bib8) 2013
Sharma (MSE_1126_1_012081bib10) 2002; 25
Hurlimann (MSE_1126_1_012081bib7); 21
Zhang (MSE_1126_1_012081bib12) 2000; 20
Rajendran (MSE_1126_1_012081bib9) 2012
References_xml – volume: 236
  start-page: 500
  year: 2013
  ident: MSE_1126_1_012081bib11
  article-title: A Parametric study of double-ceramic layer thermal barrier coatings
  publication-title: Surface and Coating Technologies
  doi: 10.1016/j.surfcoat.2013.10.049
  contributor:
    fullname: Han
– start-page: 355
  year: 2012
  ident: MSE_1126_1_012081bib9
  article-title: Gas Turbine Coatings-An overview
  contributor:
    fullname: Rajendran
– ident: MSE_1126_1_012081bib2
  contributor:
    fullname: Kang
– volume: 20
  start-page: 1809
  year: 2000
  ident: MSE_1126_1_012081bib12
  article-title: Synthesis of Mg-α SiAlON powders from talc and halolysite clay minerals
  publication-title: Journal of European ceramic society
  doi: 10.1016/S0955-2219(00)00047-9
  contributor:
    fullname: Zhang
– volume: 12
  year: 2013
  ident: MSE_1126_1_012081bib4
  publication-title: Three-point bending analyses of short fiber reinforced thermoplastics: a comparison between simulation and test results
  contributor:
    fullname: Gruber
– volume: 2
  year: 2013
  ident: MSE_1126_1_012081bib5
  publication-title: Experimental evaluation of strength and stiffness of fibre reinforced composites under flexural loading
  contributor:
    fullname: Rathnakar
– year: 2013
  ident: MSE_1126_1_012081bib8
  article-title: Analytical and Experimental Study of Residual Stresses in CFRP
  doi: 10.1155/2013/671469
  contributor:
    fullname: Chiang
– volume: 5
  year: 2013
  ident: MSE_1126_1_012081bib1
  article-title: Advanced composite materials of the future in aerospace mdustry
  publication-title: INCAS Bulletin
  contributor:
    fullname: Mrazova
– volume: 25
  start-page: 15
  year: 2002
  ident: MSE_1126_1_012081bib10
  article-title: Synthesis microstructure and mechanical properties of Ceria stabilized tetragonal Zirconia prepared by spray drying technique
  publication-title: Material Science
  contributor:
    fullname: Sharma
– start-page: 33
  year: 2014
  ident: MSE_1126_1_012081bib3
  article-title: Stress Analysis and Weight Optimization of a Wing Box Structure Subjected To Flight Loads
  contributor:
    fullname: Immanuvel
– year: 2013
  ident: MSE_1126_1_012081bib6
  contributor:
    fullname: Arunachalam
– volume: 21
  start-page: 31
  ident: MSE_1126_1_012081bib7
  article-title: Investigation of local load introduction methods in aircraft pre-design
  publication-title: Aerospace Science and Technology
  doi: 10.1016/j.ast.2011.04.008
  contributor:
    fullname: Hurlimann
SSID ssj0067440
Score 2.223719
Snippet Abstract Composite materials are becoming more important in the construction of Mechanical structures. The primary objective of this paper is to analyse the...
Composite materials are becoming more important in the construction of Mechanical structures. The primary objective of this paper is to analyse the Carbon...
SourceID proquest
crossref
SourceType Aggregation Database
StartPage 12081
SubjectTerms Aircraft
Aluminum base alloys
Carbon fiber reinforced plastics
Composite materials
Finite element method
Mathematical models
Weight reduction
Wing boxes
Wings (aircraft)
Title Correlation of CFRP and AA7075 Aircraft Wing box structure using FEM
URI https://www.proquest.com/docview/2511969285
Volume 1126
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV07T8MwELaALjAgnqK85IE1au3EsT2hUhoeUktVUdHN8iuIJS1tkfj5-PIQdGFM4um7-Ls7-7s7hG4cNyE3YXFkYuKihFsSSWFkZOPEGiG7vsuhwHk4Sh-nyfOMzeoDt1Utq2w4sSRqN7dwRt6BUFimkgp2u_iMYGoU3K7WIzS2UYtQzuGvFtlDw8QpNL8rCyJZYGIpSKPvCklf_U7OOmUNDelAEakgm95pk5xLj5MdoP06VMS9yraHaMsXR2jvTwPBY3Tfh-EalZwNz3PczyZjrAuHez0evDTufSztUudr_BaWYzP_xlW_2K-lx6B4f8fZYHiCptngtf8Y1XMRIgvhSCSoI56FQKYb5zq2knkWc2d9ADqnOskJ1SHJ0S7hXnidakZNomPDPU1dDgHKKdop5oU_Q1imgrnUEA_jNnTYjrnz1OexFYlImeNt1G3wUIuq_YUqr62FUAChAggVQKiIqiBso8sGN1Xvh5X6td75_58v0C4F1Uip8rpEOwEUfxXc_tpcl7a9Rq27wWg8CU9PL-MfhB-ogA
link.rule.ids 315,783,787,12779,21402,27938,27939,33387,33758,43614,43819
linkProvider ProQuest
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1LTwIxEG4UD-rB-Iwoag9eN9Dtdrc9GYKsqECMgcit6WuNFxYBE3--nX1EuXhte_omnfmm_WYGoVubaJ-bMBpoSmwQJYYEgmsRGBoZzUXHdRIocB6N48E0epqxWfXgtqpklbVPLBy1zQ28kbeBCotYhJzdLT4DmBoFv6vVCI1ttBNRH2igUjx9qD1xDM3vioJI5j2x4KTWd_mkr1oTs3ZRQ0PaUETKyWZ02nTORcRJD9FBRRVxt7TtEdpy82O0_6eB4Am678FwjVLOhvMM99LXF6zmFne7iY_SuPuxNEuVrfGbP451_o3LfrFfS4dB8f6O0_7oFE3T_qQ3CKq5CIEBOhLw0BLHPJHp0ExRI5hjNLHGeaCzUEUZCZVPcpSNEsedihULdaSoTlwY2wwIyhlqzPO5O0dYxJzZWBMH4zaUv46ZdaHLqOERj5lNmqhT4yEXZfsLWXxbcy4BQgkQSoBQEllC2EStGjdZ3YeV_LXexf_bN2h3MBkN5fBx_HyJ9kJQkBSKrxZqeIDclacAa31d2PkHObKovw
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Correlation+of+CFRP+and+AA7075+Aircraft+Wing+box+structure+using+FEM&rft.jtitle=IOP+conference+series.+Materials+Science+and+Engineering&rft.au=Vigneshwaran%2C+M&rft.au=Kumaran%2C+M&rft.au=Praveen%2C+kumar+K&rft.au=Revanth%2C+K&rft.date=2021-03-01&rft.pub=IOP+Publishing&rft.issn=1757-8981&rft.eissn=1757-899X&rft.volume=1126&rft.issue=1&rft_id=info:doi/10.1088%2F1757-899X%2F1126%2F1%2F012081
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1757-8981&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1757-8981&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1757-8981&client=summon