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Mechanics of Composite Materials
Erschienen in: Mechanics of Composite Materials 3/2018

09.07.2018

Finite-Layer Method: Calculation of Interface Stresses in a Composite Panel Reinforced by T-Stringers

verfasst von: A. M. Timonin

Erschienen in: Mechanics of Composite Materials | Ausgabe 3/2018

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Abstract

The finite-layer method is extended to the layered composite structures with partially bonded layers with different geometric characteristics. This makes it possible to perform a strength analysis of objects of more complex forms. The purpose of the study was to calculate the interface stresses arising in joints of composite parts and the transverse normal and tangential stresses in composite layers. Their values are necessary to estimate both the bond strength of the parts and the possibility of occurrence of internal delaminations in the composite.
Vorheriger Artikel Mechanical Behavior of a Unidirectional Basalt-Fiber-Reinforced Plastic Under Thermomechanical Loadings
Nächster Artikel Effect of Hole Machining Method on the Behavior of CFRP Laminates Under Low-Velocity Impacts

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Metadaten
Titel
Finite-Layer Method: Calculation of Interface Stresses in a Composite Panel Reinforced by T-Stringers
verfasst von
A. M. Timonin
Publikationsdatum
09.07.2018
Verlag
Springer US
Erschienen in
Mechanics of Composite Materials / Ausgabe 3/2018
Print ISSN: 0191-5665
Elektronische ISSN: 1573-8922
DOI
https://doi.org/10.1007/s11029-018-9747-3

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