MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F10%3APU92172" target="_blank" >RIV/00216305:26210/10:PU92172 - 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
MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST
Original language description
The goal of measurement was to set curves of bending moment on the wing of a small aircraft and establishing of the strain in dependence on a flight conditions. The results were used for design of the fatigue test of the connection between the center wing and outer wing.
Czech name
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Czech description
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Project
<a href="/en/project/1M0501" target="_blank" >1M0501: Aerospace Research Centre</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
27th Congress of International Council of Aeronautical Sciences
ISBN
978-0-9565333-0-2
ISSN
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e-ISSN
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Number of pages
7
Pages from-to
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Publisher name
Optimage Ltd.
Place of publication
Edinburg, UK
Event location
NICE
Event date
Sep 20, 2010
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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