Publication detail

Possibilities and methods of in-flight loading measurement

JEBÁČEK, I. HORÁK, M.

English title

Possibilities and methods of in-flight loading measurement

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

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.

Keywords in English

test, in flight, measurement

Released

2012-06-01

Publisher

Vilnius Gediminas Technical University

Location

Vilnius

ISSN

1648-7788

Journal

Aviation

Volume

16

Number

2

Pages from–to

47–50

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"
}