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JEBÁČEK, I.; HORÁK, M.
Originální název
Possibilities and methods of in-flight loading measurement
Anglický název
Druh
Článek recenzovaný mimo WoS a Scopus
Originální abstrakt
This article provides information about in-flight measurement of a small sport aircraft. Firstly the strain gauges were installed into the wing structure and then the calibration procedures were done. After the calculation of strain gauge coefficients the equations for calculating of bending moments and other variables were established. The data acquisition system was installed into the aircraft for measurement responses from strain gauges and other variables as speed, altitude, load factor and temperature. Many flights were performed with this way equipped aircraft and after that the recorded data were analyzed and those results were compared with the calculation and with the static strength tests performed before.
Anglický abstrakt
Klíčová slova
test, in flight, measurement
Klíčová slova v angličtině
Autoři
Rok RIV
2013
Vydáno
01.06.2012
Nakladatel
Vilnius Gediminas Technical University
Místo
Vilnius
ISSN
1648-7788
Periodikum
Aviation
Svazek
16
Číslo
2
Stát
Litevská republika
Strany od
47
Strany do
50
Strany počet
4
BibTex
@article{BUT94474, author="Ivo {Jebáček} and Marek {Horák}", title="Possibilities and methods of in-flight loading measurement", journal="Aviation", year="2012", volume="16", number="2", pages="47--50", issn="1648-7788" }