Delamination during buckling of composite constructional elements
DOI: https://doi.org/10.3846/aviation.2010.06Abstract
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, criterionHow to Cite
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Copyright (c) 2010 The Author(s). Published by Vilnius Gediminas Technical University.
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Copyright (c) 2010 The Author(s). Published by Vilnius Gediminas Technical University.
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This work is licensed under a Creative Commons Attribution 4.0 International License.