Publication detail

Wing bending moment measurement of TL-96 aircraft

JEBÁČEK, I.

Original Title

Wing bending moment measurement of TL-96 aircraft

Type

conference paper

Language

English

Original Abstract

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.

Keywords

measurements of the wing bending moment

Authors

JEBÁČEK, I.

RIV year

2003

Released

7. 5. 2003

Publisher

Bologna University

Location

Bologna University

ISBN

88-901080-0-2-44406

Book

2nd Youth Symposium on Experimental Solid Mechanics

Edition

NEUVEDENO

Edition number

NEUVEDENO

Pages from

107

Pages to

109

Pages count

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"
}