Publication detail

Possibilities and Methods of In Flight Loading Measurements

JEBÁČEK, I. HORÁK, M.

Original Title

Possibilities and Methods of In Flight Loading Measurements

English Title

Possibilities and Methods of In Flight Loading Measurements

Type

lecture

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.

English 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

test, in flight, measurement

Released

22.06.2011

Publisher

Iniversity of Patras

Location

Patras, GR

Pages from

1

Pages to

7

Pages count

7

Documents

BibTex


@misc{BUT75334,
  author="Ivo {Jebáček} and Marek {Horák}",
  title="Possibilities and Methods of In Flight Loading Measurements",
  annote="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.",
  address="Iniversity of Patras",
  chapter="75334",
  institution="Iniversity of Patras",
  year="2011",
  month="june",
  pages="1--7",
  publisher="Iniversity of Patras",
  type="lecture"
}