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KUNZ, J.; KOVÁŘÍK, O.; LAUSCHMANN, H.; SIEGL, J.; AUGUSTIN, P.
Originální název
Fractographic reconstitution of fatigue crack growth in integrally stiffened panels
Anglický název
Druh
Článek recenzovaný mimo WoS a Scopus
Originální abstrakt
A research program was focused on design and experimental verification of fracture marking of integrally stiffened panels during the fatigue tests under flight-by-flight spectrum loading and testing the effectiveness of various fractographic methods. The panels represent complex testing models of aircraft wing parts. Three kinds of cyclic loading were used: constant amplitude loading, flight-by-flight type spectrum loading without marking and flight-by-flight spectrum with marking. Different methods were applied for fractographic reconstitution of fatigue crack growth: a) measurement of striation spacing, b) identification of beach marks, c) image textural analysis of SEM images of fatigue fracture surfaces (textural fractography) aimed at morphological features oriented in the direction of crack growth. The obtained crack growth curves enable the study of the influence of loading spectrum on crack growth kinetics and comparison of the different fractographic methods.
Anglický abstrakt
Klíčová slova
metal fatigue, crack growth rate, fractographic reconstitution, constant amplitude loading, spectrum loading, integrally stiffened panel, high speed cutting, aircraft wing, striations, textural fractography
Klíčová slova v angličtině
Autoři
Rok RIV
2011
Vydáno
06.06.2010
Nakladatel
Elsevier Ltd.
ISSN
1877-7058
Periodikum
Procedia Engineering
Svazek
2
Číslo
1
Stát
Spojené království Velké Británie a Severního Irska
Strany od
1711
Strany do
1720
Strany počet
10
BibTex
@article{BUT50737, author="KUNZ, J. and KOVÁŘÍK, O. and LAUSCHMANN, H. and SIEGL, J. and AUGUSTIN, P.", title="Fractographic reconstitution of fatigue crack growth in integrally stiffened panels", journal="Procedia Engineering", year="2010", volume="2", number="1", pages="1711--1720" }