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JEBÁČEK, I.; HORÁK, M.
Original Title
Possibilities and methods of in-flight loading measurement
English Title
Type
Peer-reviewed article not indexed in WoS or Scopus
Original Abstract
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.
English abstract
Keywords
test, in flight, measurement
Key words in English
Authors
RIV year
2013
Released
01.06.2012
Publisher
Vilnius Gediminas Technical University
Location
Vilnius
ISBN
1648-7788
Periodical
Aviation
Volume
16
Number
2
State
Republic of Lithuania
Pages from
47
Pages to
50
Pages count
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" }