High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading

An experimental and numerical analysis of the response of laminated composite plates under high-velocity impact loads of soft body gelatine projectiles (artificial birds) is presented. The plates are exposed to tensile and compressive preloads before impact in order to cover realistic loading condit...

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Main Authors: Sebastian Heimbs, Tim Bergmann
Format: Article
Language:English
Published: Wiley 2012-01-01
Series:International Journal of Aerospace Engineering
Online Access:http://dx.doi.org/10.1155/2012/372167
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author Sebastian Heimbs
Tim Bergmann
author_facet Sebastian Heimbs
Tim Bergmann
author_sort Sebastian Heimbs
collection DOAJ
description An experimental and numerical analysis of the response of laminated composite plates under high-velocity impact loads of soft body gelatine projectiles (artificial birds) is presented. The plates are exposed to tensile and compressive preloads before impact in order to cover realistic loading conditions of representative aeronautic structures under foreign object impact. The modelling methodology for the composite material, delamination interfaces, impact projectile, and preload using the commercial finite element code Abaqus are presented in detail. Finally, the influence of prestress and of different delamination modelling approaches on the impact response is discussed and a comparison to experimental test data is given. Tensile and compressive preloading was found to have an influence on the damage pattern. Although this general behaviour could be predicted well by the simulations, further numerical challenges for improved bird strike simulation accuracy are highlighted.
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series International Journal of Aerospace Engineering
spelling doaj-art-3786564c33b44658b7d59e5021a19cd32025-02-03T01:22:17ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742012-01-01201210.1155/2012/372167372167High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike LoadingSebastian Heimbs0Tim Bergmann1Department of Structures Engineering, Production and Aeromechanics, EADS Innovation Works, Willy-Messerschmitt-Straße, 81663 Munich, GermanyDepartment of Structures Engineering, Production and Aeromechanics, EADS Innovation Works, Willy-Messerschmitt-Straße, 81663 Munich, GermanyAn experimental and numerical analysis of the response of laminated composite plates under high-velocity impact loads of soft body gelatine projectiles (artificial birds) is presented. The plates are exposed to tensile and compressive preloads before impact in order to cover realistic loading conditions of representative aeronautic structures under foreign object impact. The modelling methodology for the composite material, delamination interfaces, impact projectile, and preload using the commercial finite element code Abaqus are presented in detail. Finally, the influence of prestress and of different delamination modelling approaches on the impact response is discussed and a comparison to experimental test data is given. Tensile and compressive preloading was found to have an influence on the damage pattern. Although this general behaviour could be predicted well by the simulations, further numerical challenges for improved bird strike simulation accuracy are highlighted.http://dx.doi.org/10.1155/2012/372167
spellingShingle Sebastian Heimbs
Tim Bergmann
High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading
International Journal of Aerospace Engineering
title High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading
title_full High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading
title_fullStr High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading
title_full_unstemmed High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading
title_short High-Velocity Impact Behaviour of Prestressed Composite Plates under Bird Strike Loading
title_sort high velocity impact behaviour of prestressed composite plates under bird strike loading
url http://dx.doi.org/10.1155/2012/372167
work_keys_str_mv AT sebastianheimbs highvelocityimpactbehaviourofprestressedcompositeplatesunderbirdstrikeloading
AT timbergmann highvelocityimpactbehaviourofprestressedcompositeplatesunderbirdstrikeloading