The fatigue test effectiveness improvement using NDT methods combination

Result code in IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F09%3A%230000937" target="_blank" >RIV/00010669:_____/09:#0000937 - isvavai.cz</a>

Result on the web

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DOI - Digital Object Identifier

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Result language

angličtina

Original language name

The fatigue test effectiveness improvement using NDT methods combination

Original language description

The Experimental Strength Laboratory provides full-scale fatigue tests of aircraft structures and their components for the Czech aviation industry. Based on example of utilisation of VT, AE, UT and ET methods combination for failures detection during VUT100 aircraft wing attachment fatigue test, there is the complexity of detection illustrated and also the ability of Experimental strength NDT laboratory to solve such tasks. The utilisation of combination of NDT VT, AE, UT and ET methods significantly raises the probability of failure indication in crack inception phase, makes shorter the inspection time and in consequence whereof degreases costs connected with structure fatigue test accomplishment.

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

JL - Fatigue and fracture mechanics

OECD FORD branch

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Project

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Continuities

Z - Vyzkumny zamer (s odkazem do CEZ)

Publication year

2009

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

1/2009

Issue of the periodical within the volume

1

Country of publishing house

CZ - CZECH REPUBLIC

Number of pages

3

Pages from-to

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UT code for WoS article

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EID of the result in the Scopus database

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