Delamination during buckling of composite constructional elements

    Antanas Žiliukas Info
DOI: https://doi.org/10.3846/aviation.2010.06

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.

Kompozitinių konstrukcijų elementų atsisluoksniavimas klupdant

Santrauka. Kompozitinių konstrukcijų elementų atsisluoksniavimas nustatomas remiantis normaliniais ir tangentiniais įtempiais. Autorius siūlo netiesinį stiprumo kriterijų, įvertinantį sudėtingą įtempių būvį sprendžiant kompozitų atsisluoksniavimo problemą.

Reikšminiai žodžiai: atsisluoksniavimas, kompozitas, stiprumo kriterijus.

First publish online: 14 Oct 2010

Keywords:

delamination, composite, strength, criterion

How to Cite

Žiliukas, A. (2010). Delamination during buckling of composite constructional elements. Aviation, 14(2), 38-42. https://doi.org/10.3846/aviation.2010.06

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June 30, 2010
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2010-06-30

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How to Cite

Žiliukas, A. (2010). Delamination during buckling of composite constructional elements. Aviation, 14(2), 38-42. https://doi.org/10.3846/aviation.2010.06

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