Experimental verification of thickness effect on fatigue crack growth in AA 2124 plate
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F18%3AN0000051" target="_blank" >RIV/00010669:_____/18:N0000051 - isvavai.cz</a>
Result on the web
<a href="http://experimentalni-mechanika.cz/konference/konference/2018.html" target="_blank" >http://experimentalni-mechanika.cz/konference/konference/2018.html</a>
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Experimental verification of thickness effect on fatigue crack growth in AA 2124 plate
Original language description
Both predictions and experimental results indicate for some materials significant discrepancies between crack propagation data of machined parts from a thick plate to different thinner thicknesses. The different fatigue crack growth behavior under constant and variable amplitude loading can be recognized. The thickness influence could be one of the main possible reasons for this unexpected behavior. The paper deals with a plate thickness of 50 mm made from 2124 T851 aluminum alloy. Crack propagation was investigated for various specimen thicknesses and different loading conditions. No significant thickness influence on the crack propagation behavior occurred both for constant and variable amplitude loading typical for a commuter aircraft loading spectra. It implies that present prediction models are able to predict the crack propagation in this material only using basic material characteristics defined under the constant amplitude loading.
Czech name
—
Czech description
—
Classification
Type
D - Article in proceedings
CEP classification
—
OECD FORD branch
20301 - Mechanical engineering
Result continuities
Project
<a href="/en/project/TE02000032" target="_blank" >TE02000032: Advanced Aerostructures Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2018
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Article name in the collection
Experimental Stress Analysis - 56th International Scientific Conference, EAN 2018 - Conference Proceedings
ISBN
978-80-270-4062-9
ISSN
—
e-ISSN
—
Number of pages
6
Pages from-to
347-352
Publisher name
Czech Society for Mechanics
Place of publication
Liberec
Event location
Harrachov
Event date
Jun 5, 2018
Type of event by nationality
EUR - Evropská akce
UT code for WoS article
—