Detail publikace

Fatigue crack initiation and early growth in glare 3 fiber-metal laminate subjected to mixed tensile and bending loading

HEGER, J. CHLUPOVÁ, A. VAŠEK, A.

Anglický název

Fatigue crack initiation and early growth in glare 3 fiber-metal laminate subjected to mixed tensile and bending loading

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

Originální abstrakt

A special open-hole sheet specimen from GLARE fiber metal laminate was used to simulate the mixed type of loading similar to the loading of a riveted hole in a real fuselage skin structure. The effect of cyclic tension and secondary bending loading was studied. The number of cycles to the crack initiation was measured and the crack growth rate in the surface layer of the laminate was evaluated.

Vydáno

2001-06-01

Nakladatel

University of Glasgow Print Unit

Místo

Glasgow (Scotland)

ISBN

0-85261-731-3

Kniha

Second International Conference on Advanced Engineering Design

Strany od–do

15–

Počet stran

6

BIBTEX


@inproceedings{BUT5965,
  author="Jaromír {Heger} and Alice {Chlupová} and Alois {Vašek}",
  title="Fatigue crack initiation and early growth in glare 3 fiber-metal laminate subjected to mixed tensile and bending loading",
  booktitle="Second International Conference on Advanced Engineering Design",
  year="2001",
  pages="6",
  publisher="University of Glasgow Print Unit",
  address="Glasgow (Scotland)",
  isbn="0-85261-731-3"
}