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AUGUSTIN, P.
Originální název
Simulation of Fatigue Crack Growth in the High Speed Machined Panel under the Constant Amplitude and Spectrum Loading
Typ
článek ve sborníku ve WoS nebo Scopus
Jazyk
angličtina
Originální abstrakt
The paper describes methodology of numerical simulation of fatigue crack growth under the constant amplitude and spectrum loading and its application on integrally stiffened panels made of 2024-T351 aluminium alloy using high speed cutting technique. Presented approach is based on the calculation of stress intensity factor function from finite element results, subsequent crack growth analyses were performed in NASGRO. For predictions of crack growth under the spectrum loading a sequence representing service loading of the transport airplane wing was prepared. Three crack growth models were applied: non-interaction, Willenborg and Strip Yield. Relatively large experimental program comprising both the constant amplitude and spectrum tests on integral panels and CCT specimens was undertaken in order to acquire crack growth rate data and enable verification of simulations.
Klíčová slova
fatigue, fracture mechanics, crack growth, spectrum loading, integrally stiffened panels
Autoři
Rok RIV
2009
Vydáno
27. 5. 2009
Nakladatel
Springer Science+Business Media
Místo
Dodrecht
ISBN
978-90-481-2745-0
Kniha
Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue
Strany od
1005
Strany do
1018
Strany počet
14
BibTex
@inproceedings{BUT33052, author="Petr {Augustin}", title="Simulation of Fatigue Crack Growth in the High Speed Machined Panel under the Constant Amplitude and Spectrum Loading", booktitle="Proceedings of the 25th Symposium of the International Committee on Aeronautical Fatigue", year="2009", pages="1005--1018", publisher="Springer Science+Business Media", address="Dodrecht", isbn="978-90-481-2745-0" }