Probability of Detection and Prediction of Fatigue Crack Growth in Aircraft Structures
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001032" target="_blank" >RIV/00010669:_____/10:#0001032 - isvavai.cz</a>
Result on the web
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DOI - Digital Object Identifier
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Alternative languages
Result language
angličtina
Original language name
Probability of Detection and Prediction of Fatigue Crack Growth in Aircraft Structures
Original language description
The paper describes possibilities of nondestructive inspection and computing procedures for assessings fatigue damage of commuter aircraft?s principal structural elements. Nondestructive inspection provides crack detection and limits for minimal detectable crack size for the method studied. Computing provides numerical calculation of fatigue crack growth.
Czech name
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Czech description
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Classification
Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JL - Fatigue and fracture mechanics
OECD FORD branch
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Result continuities
Project
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Continuities
Z - Vyzkumny zamer (s odkazem do CEZ)
Others
Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Name of the periodical
Czech Aerospace Proceedings / Letecký zpravodaj
ISSN
1211-877X
e-ISSN
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Volume of the periodical
3/2010
Issue of the periodical within the volume
3
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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