Initial failure of mechanically fastened joints with offset loading: Advanced Composites Letters

Brian G Falzon; Glyn AO Davies

doi:10.1177/096369359700600401

Initial failure of mechanically fastened joints with offset loading: Advanced Composites Letters

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Abstract

In this preliminary study the initial failure of a bolted composite joint was investigated. The results of an experimental program using two simple beams bolted together with offset loading are presented. These test specimens were used to simulate a typical skin-spar attachment in a composite wing undergoing hydraulic shock. Initial failure was found to be due to a prying force induced at the outer sections of the joint leading to transverse shear failure.

Original language	English
Pages (from-to)	91-94
Number of pages	4
Journal	Adv. Compos. Lett.
Volume	6
Issue number	4
DOIs	https://doi.org/10.1177/096369359700600401
Publication status	Published - 1997

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@article{a8262bebdfb64a7480dafad28ea58e6a,

title = "Initial failure of mechanically fastened joints with offset loading: Advanced Composites Letters",

abstract = "In this preliminary study the initial failure of a bolted composite joint was investigated. The results of an experimental program using two simple beams bolted together with offset loading are presented. These test specimens were used to simulate a typical skin-spar attachment in a composite wing undergoing hydraulic shock. Initial failure was found to be due to a prying force induced at the outer sections of the joint leading to transverse shear failure.",

author = "Falzon, {Brian G} and Davies, {Glyn AO}",

year = "1997",

doi = "10.1177/096369359700600401",

language = "English",

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journal = "Adv. Compos. Lett.",

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publisher = "SAGE Publications Ltd",

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AU - Falzon, Brian G

AU - Davies, Glyn AO

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AB - In this preliminary study the initial failure of a bolted composite joint was investigated. The results of an experimental program using two simple beams bolted together with offset loading are presented. These test specimens were used to simulate a typical skin-spar attachment in a composite wing undergoing hydraulic shock. Initial failure was found to be due to a prying force induced at the outer sections of the joint leading to transverse shear failure.

U2 - 10.1177/096369359700600401

DO - 10.1177/096369359700600401

M3 - Article

SN - 0963-6935

VL - 6

SP - 91

EP - 94

JO - Adv. Compos. Lett.

JF - Adv. Compos. Lett.

IS - 4

ER -

Initial failure of mechanically fastened joints with offset loading: Advanced Composites Letters

Abstract

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