Fatigue Crack Growth Test of the Built-up Panel in Section 22-23
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F16%3APU123107" target="_blank" >RIV/00216305:26210/16:PU123107 - 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
Fatigue Crack Growth Test of the Built-up Panel in Section 22-23
Original language description
The report deals with the description of experimental set-up, procedure and results of fatigue crack growth test and residual strength test of the built-up panel representing L 410 NG bottom wing panel in section 22-23.
Czech name
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Czech description
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Classification
Type
V<sub>souhrn</sub> - Summary research report
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
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Result continuities
Project
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Continuities
N - Vyzkumna aktivita podporovana z neverejnych zdroju
Others
Publication year
2016
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Number of pages
101
Place of publication
Neuveden
Publisher/client name
Neuveden
Version
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