Detail publikace

Possibilities and methods of in-flight loading measurement

JEBÁČEK, I. HORÁK, M.

Anglický název

Possibilities and methods of in-flight loading measurement

Typ

Článek recenzovaný mimo WoS a Scopus

Jazyk

en

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.

Klíčová slova anglicky

test, in flight, measurement

Vydáno

2012-06-01

Nakladatel

Vilnius Gediminas Technical University

Místo

Vilnius

ISSN

1648-7788

Časopis

Aviation

Ročník

16

Číslo

2

Strany od–do

47–50

Počet stran

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"
}