Damage tolerance analysis of a complex aircraft part

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F14%3A%230001717" target="_blank" >RIV/00010669:_____/14:#0001717 - isvavai.cz</a>

Result on the web

<a href="http://www.czaerospace.eu/en/2014-02-50.html" target="_blank" >http://www.czaerospace.eu/en/2014-02-50.html</a>

DOI - Digital Object Identifier

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Result language

angličtina

Original language name

Damage tolerance analysis of a complex aircraft part

Original language description

The purpose of this paper is to describe the application of an analytical and numerical technique for the analysis of global structure. The prediction and assessment of fatigue crack propagation in real engineering structures and components must considerrealistic boundary conditions. The article compared the application of the FASTRAN retardation model with a load sequence simulating the real operation of an aircraft structure. Stress state analysis is performed using FEM numerical simulation of the global FEM model, including the boundary conditions around the failure investigation.

Czech name

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Czech description

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Type

J_x - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)

CEP classification

JI - Composite materials

OECD FORD branch

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Project

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Continuities

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Publication year

2014

Confidentiality

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Name of the periodical

Czech Aerospace Proceedings / Letecký zpravodaj

ISSN

1211-877X

e-ISSN

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Volume of the periodical

2/2014

Issue of the periodical within the volume

2

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

4

Pages from-to

28-31

UT code for WoS article

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EID of the result in the Scopus database

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