Failure Analysis of Carbon Fiber Laminate Aircraft Strut Model

Kód výsledku v IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F46747885%3A24220%2F20%3A00008279" target="_blank" >RIV/46747885:24220/20:00008279 - isvavai.cz</a>
Výsledek na webu
<a href="https://www.engmech.cz/im/im/page/proc" target="_blank" >https://www.engmech.cz/im/im/page/proc</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.21495/5896-3-516" target="_blank" >10.21495/5896-3-516</a>

Jazyk výsledku
angličtina
Název v původním jazyce
Failure Analysis of Carbon Fiber Laminate Aircraft Strut Model
Popis výsledku v původním jazyce
The aim of this work is to verify functionality of an aircraft strut made of carbon fiber laminate. This goal was achieved in several steps. The aircraft strut model was manufactured and used for two types of mechanical tests. Prior to the tests, FEM simulations had been executed. The simulations predicted the failure mechanism correctly and offered good estimation of critical load. The functionality of the aircraft strut was verified.
Název v anglickém jazyce
Failure Analysis of Carbon Fiber Laminate Aircraft Strut Model
Popis výsledku anglicky
The aim of this work is to verify functionality of an aircraft strut made of carbon fiber laminate. This goal was achieved in several steps. The aircraft strut model was manufactured and used for two types of mechanical tests. Prior to the tests, FEM simulations had been executed. The simulations predicted the failure mechanism correctly and offered good estimation of critical load. The functionality of the aircraft strut was verified.

Rok uplatnění
2020
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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