Wing bending moment measurement of TL-96 aircraft

Kód výsledku v 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>
Výsledek na webu
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DOI - Digital Object Identifier
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Jazyk výsledku
angličtina
Název v původním jazyce
Wing bending moment measurement of TL-96 aircraft
Popis výsledku v původním jazyce
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.
Název v anglickém jazyce
Wing bending moment measurement of TL-96 aircraft
Popis výsledku anglicky
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.

Projekt
<a href="/cs/project/LN00B051" target="_blank" >LN00B051: Centrum leteckého a kosmického výzkumu (CLKV)</a><br>
Návaznosti
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Rok uplatnění
2003
Kód důvěrnosti údajů
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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