Failure Analysis of Carbon Fiber Laminate Aircraft Strut Model
The result's identifiers
Result code in 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>
Result on the web
<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>
Alternative languages
Result language
angličtina
Original language name
Failure Analysis of Carbon Fiber Laminate Aircraft Strut Model
Original language description
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.
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
CEP classification
—
OECD FORD branch
21100 - Other engineering and technologies
Result continuities
Project
—
Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2020
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Engineering Mechanics 2020
ISBN
978-80-214-5896-3
ISSN
1805-8248
e-ISSN
—
Number of pages
4
Pages from-to
516-519
Publisher name
BRNO UNIV TECHNOL, FAC MECHANICAL ENGINEERING
Place of publication
Brno
Event location
online
Event date
Jan 1, 2020
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
000667956100121