Detail publikace

Wing bending moment measurement of TL-96 aircraft

JEBÁČEK, I.

Originální název

Wing bending moment measurement of TL-96 aircraft

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

This papers describes the measurements of the wing bending moment of ultra light aircraft TL-96 Star. The bending moment was obtained by a series of strain gauges installed in the cantilevers of wings. Basic parameters such as, flight load factor, speed, altitude and electrical response of strain gages, were recorded by the data acquisition system DAS 12. Then the recorded data was analysed. The results of this analysis were the bending moments of the wings. The measured bending moments were compared with the computed results.

Klíčová slova

measurements of the wing bending moment

Autoři

JEBÁČEK, I.

Rok RIV

2003

Vydáno

7. 5. 2003

Nakladatel

Bologna University

Místo

Bologna University

ISBN

88-901080-0-2-44406

Kniha

2nd Youth Symposium on Experimental Solid Mechanics

Edice

NEUVEDENO

Číslo edice

NEUVEDENO

Strany od

107

Strany do

109

Strany počet

2

BibTex

@inproceedings{BUT7280,
  author="Ivo {Jebáček}",
  title="Wing bending moment measurement of TL-96 aircraft",
  booktitle="2nd Youth Symposium on Experimental Solid Mechanics",
  year="2003",
  pages="107--109",
  publisher="Bologna University",
  address="Bologna University",
  isbn="88-901080-0-2-44406"
}