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Delamination during buckling of composite constructional elements

    Antanas Žiliukas Affiliation

Abstract

Laminated constructional elements have widespread applications in aerospace. This paper presents of the buckling for E‐Glass. Design solution based by the criteria of strength materials. The delamination of composite constructional elements is determined by the normal and shear stress. The non‐linear strength criterion suggested by the author in case of complex state of stress.


Santrauka


Kompozitiniu konstrukciju elementu atsisluoksniavimas nustatomas remiantis normaliniais ir tangentiniais itempiais. Autorius siūlo netiesini stiprumo kriteriju, ivertinanti sudetinga itempiu būvi sprendžiant kompozitu atsisluoksniavimo problema.


First Publish Online: 14 Oct 2010


Reikšminiai žodžiai: atsisluoksniavimas, kompozitas, stiprumo kriterijus

Keyword : delamination, composite, strength, criterion

How to Cite
[1]
Žiliukas, A. 2010. Delamination during buckling of composite constructional elements. Aviation. 14, 2 (Jun. 2010), 38-42. DOI:https://doi.org/10.3846/aviation.2010.06.
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Jun 30, 2010
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This work is licensed under a Creative Commons Attribution 4.0 International License.