Analysis of Bonded Composite Patch Using FEM
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F60162694%3AG43__%2F08%3A00424138" target="_blank" >RIV/60162694:G43__/08:00424138 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Analysis of Bonded Composite Patch Using FEM
Original language description
The aim of the work is to create a FEM model of bonded composite patch. The tension is put on analysing the adhesive shear stress that is crucial for the load capacity of the bonded joint. Included are influencing factors like adhesive fillet, thicknessof the patch, the length of damage, symmetry of the joint and a chamfer of damaged plate. The goals of the work help to battle aircraft repairing in the field conditions.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
KA - Militarism
OECD FORD branch
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Result continuities
Project
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Continuities
S - Specificky vyzkum na vysokych skolach
Others
Publication year
2008
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Acta Avionica
ISSN
1335-9479
e-ISSN
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Volume of the periodical
10
Issue of the periodical within the volume
16
Country of publishing house
CZ - CZECH REPUBLIC
Number of pages
4
Pages from-to
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UT code for WoS article
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EID of the result in the Scopus database
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