Fatigue test of flap hinge made of castaluminum alloy (LU7-2017-COC.ZK)
The result's identifiers
Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F17%3APU136333" target="_blank" >RIV/00216305:26210/17:PU136333 - isvavai.cz</a>
Result on the web
—
DOI - Digital Object Identifier
—
Alternative languages
Result language
angličtina
Original language name
Fatigue test of flap hinge made of castaluminum alloy (LU7-2017-COC.ZK)
Original language description
The report deals with the description of experimental set-up, procedure and results of fatigue tests of L 410 NG flap hinge on a fuselage.
Czech name
—
Czech description
—
Classification
Type
V<sub>souhrn</sub> - Summary research report
CEP classification
—
OECD FORD branch
20304 - Aerospace engineering
Result continuities
Project
<a href="/en/project/TE02000032" target="_blank" >TE02000032: Advanced Aerostructures Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)
Others
Publication year
2017
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů
Data specific for result type
Number of pages
41
Place of publication
Neuveden
Publisher/client name
Neuveden
Version
—