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AUGUSTIN, P.
Original Title
Simulation of Fatigue Crack Growth in Integrally Stiffened Panels under the Constant Amplitude and Spectrum Loading
Type
conference paper
Language
English
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
fatigue, fracture mechanics, crack growth, spectrum loading, integrally stiffened panels
Authors
RIV year
2009
Released
31. 12. 2009
Publisher
Institute of Aviation
Location
Warsaw
ISBN
978-83-929922-1-9
Book
Fatigue of Aircraft Structures
Edition
Monographic Series
Edition number
Issue 2009
Pages from
5
Pages to
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" }