Publication detail
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading
AUGUSTIN, P.
English title
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading
Type
Paper in proceedings (conference paper)
Language
en
Original abstract
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.
Keywords in English
fatigue, fracture mechanics, crack growth, spectrum loading, integrally stiffened panels
Released
2009-12-31
Publisher
Institute of Aviation
Location
Warsaw
ISBN
978-83-929922-1-9
Book
Fatigue of Aircraft Structures
Pages from–to
5–19
Pages count
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"
}