2016
DOI: 10.5604/12314005.1213520
|View full text |Cite
|
Sign up to set email alerts
|

An Application of Stiffness Matrix Method to Determining of Dispersion Curves for Arbitrary Composite Materials

Abstract: Nowadays multi-layered composite material is very often applied in different kind of structures, like aircrafts, boats or vehicles. Parts of structures, which are made of these materials, are significantly lighter in comparison with traditional materials, like aluminum or steel alloys. On the other hand, the process of damage creation and evolution in the case of composites is much more complex. Moreover, the damages, which are characteristic for multi-layered materials (matrix cracking, fibre breakage, delami… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2017
2017
2023
2023

Publication Types

Select...
3

Relationship

1
2

Authors

Journals

citations
Cited by 3 publications
(1 citation statement)
references
References 14 publications
0
1
0
Order By: Relevance
“…Therefore, the main aim of this work is to estimate the dispersion curves for the composites, which consist of this kind of layer materials, namely fibers with epoxy resin (CFRP, Fibers T300, Matrix N5208) and aluminum alloy PA38. Moreover, the present work should be considered as the continuation of the previous studies (Barski and Pająk, 2016). In that paper the dispersion curves obtained for a single lamina and for a multilayered composite material with quasiisotropic mechanical properties are presented.…”
Section: Introductionmentioning
confidence: 71%
“…Therefore, the main aim of this work is to estimate the dispersion curves for the composites, which consist of this kind of layer materials, namely fibers with epoxy resin (CFRP, Fibers T300, Matrix N5208) and aluminum alloy PA38. Moreover, the present work should be considered as the continuation of the previous studies (Barski and Pająk, 2016). In that paper the dispersion curves obtained for a single lamina and for a multilayered composite material with quasiisotropic mechanical properties are presented.…”
Section: Introductionmentioning
confidence: 71%