Computational Analysis of Flight Deck Structural Behaviour under Variable Loadings

The flight deck of an aircraft carrier is subjected to various loads. In addition, the operation of fixed-wing aircraft presents unique structural requirements for the deck. This paper, therefore, compares the structural behaviour of a flight deck which was designed following the guidelines of three...

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Main Authors: Victoria G. Carter, Md Jahir Rizvi
Format: Article
Language:English
Published: MDPI AG 2021-11-01
Series:Journal of Marine Science and Engineering
Subjects:
Online Access:https://www.mdpi.com/2077-1312/9/11/1262
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author Victoria G. Carter
Md Jahir Rizvi
author_facet Victoria G. Carter
Md Jahir Rizvi
author_sort Victoria G. Carter
collection DOAJ
description The flight deck of an aircraft carrier is subjected to various loads. In addition, the operation of fixed-wing aircraft presents unique structural requirements for the deck. This paper, therefore, compares the structural behaviour of a flight deck which was designed following the guidelines of three classification societies: Lloyd’s Register (LR), Det Norske Veritas Germanischer Lloyd (DNV), and Registro Italiano Navale (RINA). The loading scenarios considered in this work represent the operation of an F-35B Lightning jet from a Queen Elizabeth-class (QEC) aircraft carrier. A commercial finite element analysis (FEA) software ANSYS was also used to investigate the deflection, stress and strain on the deck plates. The analysis identified that only the calculated deck thickness values based on the LR regulations would meet the requirement for the class. This finding was further supported by the FEA.
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spelling doaj.art-4725d617da5542dea99439295cda64ef2023-11-22T23:54:07ZengMDPI AGJournal of Marine Science and Engineering2077-13122021-11-01911126210.3390/jmse9111262Computational Analysis of Flight Deck Structural Behaviour under Variable LoadingsVictoria G. Carter0Md Jahir Rizvi1School of Engineering, Computing and Mathematics, Faculty of Science and Engineering, University of Plymouth, Plymouth PL4 8AA, UKSchool of Engineering, Computing and Mathematics, Faculty of Science and Engineering, University of Plymouth, Plymouth PL4 8AA, UKThe flight deck of an aircraft carrier is subjected to various loads. In addition, the operation of fixed-wing aircraft presents unique structural requirements for the deck. This paper, therefore, compares the structural behaviour of a flight deck which was designed following the guidelines of three classification societies: Lloyd’s Register (LR), Det Norske Veritas Germanischer Lloyd (DNV), and Registro Italiano Navale (RINA). The loading scenarios considered in this work represent the operation of an F-35B Lightning jet from a Queen Elizabeth-class (QEC) aircraft carrier. A commercial finite element analysis (FEA) software ANSYS was also used to investigate the deflection, stress and strain on the deck plates. The analysis identified that only the calculated deck thickness values based on the LR regulations would meet the requirement for the class. This finding was further supported by the FEA.https://www.mdpi.com/2077-1312/9/11/1262flight deckaircraft carrierfailure behaviourstressdeformationFEA
spellingShingle Victoria G. Carter
Md Jahir Rizvi
Computational Analysis of Flight Deck Structural Behaviour under Variable Loadings
Journal of Marine Science and Engineering
flight deck
aircraft carrier
failure behaviour
stress
deformation
FEA
title Computational Analysis of Flight Deck Structural Behaviour under Variable Loadings
title_full Computational Analysis of Flight Deck Structural Behaviour under Variable Loadings
title_fullStr Computational Analysis of Flight Deck Structural Behaviour under Variable Loadings
title_full_unstemmed Computational Analysis of Flight Deck Structural Behaviour under Variable Loadings
title_short Computational Analysis of Flight Deck Structural Behaviour under Variable Loadings
title_sort computational analysis of flight deck structural behaviour under variable loadings
topic flight deck
aircraft carrier
failure behaviour
stress
deformation
FEA
url https://www.mdpi.com/2077-1312/9/11/1262
work_keys_str_mv AT victoriagcarter computationalanalysisofflightdeckstructuralbehaviourundervariableloadings
AT mdjahirrizvi computationalanalysisofflightdeckstructuralbehaviourundervariableloadings