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KUNZ, J.; KOVÁŘÍK, O.; LAUSCHMANN, H.; SIEGL, J.; AUGUSTIN, P.
Original Title
Fractographic reconstitution of fatigue crack growth in integrally stiffened panels
English Title
Type
Peer-reviewed article not indexed in WoS or Scopus
Original Abstract
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.
English abstract
Keywords
metal fatigue, crack growth rate, fractographic reconstitution, constant amplitude loading, spectrum loading, integrally stiffened panel, high speed cutting, aircraft wing, striations, textural fractography
Key words in English
Authors
RIV year
2011
Released
06.06.2010
Publisher
Elsevier Ltd.
ISBN
1877-7058
Periodical
Procedia Engineering
Volume
2
Number
1
State
United Kingdom of Great Britain and Northern Ireland
Pages from
1711
Pages to
1720
Pages count
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" }