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LAP Lambert Academic Publishing Bolted Joints in Laminated Composites

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£59.00 £57.69 £57.98 £58.26 £58.55 £58.83 £59.12 08 April 2026 28 April 2026 19 May 2026 08 June 2026 29 June 2026

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Description

Laminated composites are now extensively used in aircraft structures. Bolted joints remain the primary means of joining composite components in modern aircraft structures. The high stress concentration at the contact between the bolt and the hole and the nature of the composite material itself give the research in bolted joint in composite structures great importance through the recent 30 years. The main objective of our study is to to find out the effect of various joining and geometrical parameters upon the bearing strength of the laminated composite plate. To achieve this goal, a numerical model which has the capability of predicting the bearing strength for the composite bolted joint problem was introduced. Results showed that the bearing strength increased as the friction coefficient and the washer size increased and decreased as the clearance increased. About the Author Since 2002, Tamer is working as a teacher/research assistant in the Zagazig University in Egypt and Universitat de Girona of Spain. His main interest is the damage tolerance of aeronautical laminated composites.

Product Specifications

Format
paperback
Domain
Amazon UK
Release Date
16 February 2013
Listed Since
21 February 2013

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