Fatigue crack initiation and early growth in glare 3 fiber-metal laminate subjected to mixed tensile and bending loading

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F01%3APU21977" target="_blank" >RIV/00216305:26210/01:PU21977 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Fatigue crack initiation and early growth in glare 3 fiber-metal laminate subjected to mixed tensile and bending loading
Original language description
A special open-hole sheet specimen from GLARE fiber metal laminate was used to simulate the mixed type of loading similar to the loading of a riveted hole in a real fuselage skin structure. The effect of cyclic tension and secondary bending loading was studied. The number of cycles to the crack initiation was measured and the crack growth rate in the surface layer of the laminate was evaluated.
Czech name
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Czech description
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Project
Result was created during the realization of more than one project. More information in the Projects tab.
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2001
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Second International Conference on Advanced Engineering Design
ISBN
0 85261 731 3
ISSN
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e-ISSN
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Number of pages
6
Pages from-to
15-20
Publisher name
University of Glasgow Print Unit
Place of publication
Glasgow (Scotland)
Event location
Glagow
Event date
Jun 24, 2001
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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