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Description
  • The purpose of this paper is to describe the technique of modelling fasteners using FEM and to demonstrate its accuracy and capability by examining some examples of practical significance such as the connection of skins on the lower side of wing of small transport aircraft and the global modelling of a mechanical joint connecting metal and composite parts with or without additional bonding. The consideration of fastener stiffness during stress analysis is an integral part of the damage tolerance philosophy for both old new aircraft designs.
  • The purpose of this paper is to describe the technique of modelling fasteners using FEM and to demonstrate its accuracy and capability by examining some examples of practical significance such as the connection of skins on the lower side of wing of small transport aircraft and the global modelling of a mechanical joint connecting metal and composite parts with or without additional bonding. The consideration of fastener stiffness during stress analysis is an integral part of the damage tolerance philosophy for both old new aircraft designs. (en)
Title
  • Practical application of FEM to determine the effect of mechanical fasteners on stress state and fatigue behavior ofaircraft structure
  • Practical application of FEM to determine the effect of mechanical fasteners on stress state and fatigue behavior ofaircraft structure (en)
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  • Practical application of FEM to determine the effect of mechanical fasteners on stress state and fatigue behavior ofaircraft structure
  • Practical application of FEM to determine the effect of mechanical fasteners on stress state and fatigue behavior ofaircraft structure (en)
skos:notation
  • RIV/00010669:_____/13:#0001556!RIV14-MPO-00010669
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  • I
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http://linked.open...iv/duvernostUdaju
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  • 98192
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  • RIV/00010669:_____/13:#0001556
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  • Finite Element Method; Fastener; Crack (en)
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  • [4FB8A5692F22]
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  • Conference Proceedings of3rd International Conference of Engineering Against Failure
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  • Doubrava, Radek
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issn
  • 2241-5890
number of pages
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  • Laboratory of Technology & Strength of Materials (LTSM) Department of Mechanical Engineering and Aeronautics - University Campus 26500 Rion – Patras
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  • 978-960-88104-3-3
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