The advanced fatigue strength test method of thin-walled small aircraft wing
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00010669%3A_____%2F10%3A%230001027" target="_blank" >RIV/00010669:_____/10:#0001027 - 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
The advanced fatigue strength test method of thin-walled small aircraft wing
Original language description
Nowadays the production and operation of small sport and ultralight aircraft is increasing. The number of fatal accidents of these aircraft is increasing too. One of causes of disconsolate situation from point of view operational safety is a gap of acceptable and cost effective certification methods of strength reliability. The procedures during preparation and realisation certification fatigue test of thin-walled wing structure of KP-5-ASA aircraft are used for advanced fatigue certification test method development
Czech name
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Czech description
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Classification
Type
D - Article in proceedings
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
Article name in the collection
Danubia ? Adria 27th Symposium on Advances in Experimental Mechanics
ISBN
978-83-87982-59-1
ISSN
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e-ISSN
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Number of pages
2
Pages from-to
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Publisher name
Institute of Machines Design an Operation
Place of publication
Wroclaw
Event location
Wroclaw University of Technology,
Event date
Jan 1, 2010
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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