Delamination during buckling of composite constructional elements
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‐line...
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| Format: | Article |
| Language: | English |
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Vilnius Gediminas Technical University
2010-06-01
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| Series: | Aviation |
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| Online Access: | https://www.tede.vgtu.lt/index.php/Aviation/article/view/5673 |
| Summary: | 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
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| ISSN: | 1648-7788 1822-4180 |