Detail publikace

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

AUGUSTIN, P.

Originální název

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

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

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

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

Autoři

AUGUSTIN, P.

Rok RIV

2009

Vydáno

31. 12. 2009

Nakladatel

Institute of Aviation

Místo

Warsaw

ISBN

978-83-929922-1-9

Kniha

Fatigue of Aircraft Structures

Edice

Monographic Series

Číslo edice

Issue 2009

Strany od

5

Strany do

19

Strany počet

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"
}