Detail publikace

Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading

AUGUSTIN, P.

Anglický název

Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

Originální abstrakt

The methodology of fatigue crack growth simulation based on the calculation of stress intensity factor function from finite element results, subsequent crack growth analysis performed in NASGRO and application on integrally stiffened wing panels are described. Large experimental program comprising both the constant amplitude and spectrum tests on integral panels and CCT specimens was undertaken in order to enable verification of simulations.

Klíčová slova anglicky

fatigue, fracture mechanics, crack growth, spectrum loading, integrally stiffened panels

Vydáno

2009-12-31

Nakladatel

Institute of Aviation

Místo

Warsaw

ISBN

978-83-929922-1-9

Kniha

Fatigue of Aircraft Structures

Strany od–do

5–19

Počet stran

14

BIBTEX


@inproceedings{BUT29262,
  author="Petr {Augustin}",
  title="Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading",
  booktitle="Fatigue of Aircraft Structures",
  year="2009",
  series="Monographic Series",
  number="Issue 2009",
  pages="5--19",
  publisher="Institute of Aviation",
  address="Warsaw",
  isbn="978-83-929922-1-9"
}