Wing bending moment measurement of TL-96 aircraft

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216305%3A26210%2F03%3APU36511" target="_blank" >RIV/00216305:26210/03:PU36511 - 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
Wing bending moment measurement of TL-96 aircraft
Original language description
This papers describes the measurements of the wing bending moment of ultra light aircraft TL-96 Star. The bending moment was obtained by a series of strain gauges installed in the cantilevers of wings. Basic parameters such as, flight load factor, speed,altitude and electrical response of strain gages, were recorded by the data acquisition system DAS 12. Then the recorded data was analysed. The results of this analysis were the bending moments of the wings. The measured bending moments were compared wiith the computed results.
Czech name
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Czech description
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Project
<a href="/en/project/LN00B051" target="_blank" >LN00B051: Aerospace research centre (ARC)</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2003
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
2nd Youth Symposium on Experimental Solid Mechanics
ISBN
88-901080-02-44
ISSN
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e-ISSN
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Number of pages
2
Pages from-to
107-108
Publisher name
Neuveden
Place of publication
Neuveden
Event location
Marino Maritima
Event date
May 7, 2003
Type of event by nationality
WRD - Celosvětová akce
UT code for WoS article
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