Publication detail

Fractographic reconstitution of fatigue crack growth in integrally stiffened panels

KUNZ, J. KOVÁŘÍK, O. LAUSCHMANN, H. SIEGL, J. AUGUSTIN, P.

English title

Fractographic reconstitution of fatigue crack growth in integrally stiffened panels

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

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.

Keywords in English

metal fatigue, crack growth rate, fractographic reconstitution, constant amplitude loading, spectrum loading, integrally stiffened panel, high speed cutting, aircraft wing, striations, textural fractography

Released

2010-06-06

Publisher

Elsevier Ltd.

ISSN

1877-7058

Journal

Procedia Engineering

Volume

2

Number

1

Pages from–to

1711–1720

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"
}