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Computational analysis of temperature effect in composite bolted joints for aeronautical applications

✍ Scribed by Santiuste, Carlos (author);Barbero, Enrique (author);Miguélez, María Henar (author)

Book ID
121463341
Publisher
SAGE Publications
Year
2010
Tongue
English
Weight
471 KB
Volume
30
Category
Article
ISSN
0731-6844

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It is well known that geometric nonlinear effects have to be taken into account when the ultimate strength of single lap composite joints are studied. In the present paper we investigate for which level of loads or prescribed end displacements nonlinear effects become significant and how they appear