Detail publikace

Possibilities and methods of in-flight loading measurement

JEBÁČEK, I. HORÁK, M.

Originální název

Possibilities and methods of in-flight loading measurement

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

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

test, in flight, measurement

Autoři

JEBÁČEK, I.; HORÁK, M.

Rok RIV

2012

Vydáno

1. 6. 2012

Nakladatel

Vilnius Gediminas Technical University

Místo

Vilnius

ISSN

1648-7788

Periodikum

AVIATION

Ročník

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"
}