Publication result detail

MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST

JEBÁČEK, I.

Original Title

MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST

English Title

MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST

Type

Paper in proceedings (conference paper)

Original Abstract

The goal of measurement was to set curves of bending moment on the wing of a small aircraft and establishing of the strain in dependence on a flight conditions. The results were used for design of the fatigue test of the connection between the center wing and outer wing.

English abstract

The goal of measurement was to set curves of bending moment on the wing of a small aircraft and establishing of the strain in dependence on a flight conditions. The results were used for design of the fatigue test of the connection between the center wing and outer wing.

Keywords

test, in flight, measurement, bending moment, fatigue

Key words in English

test, in flight, measurement, bending moment, fatigue

Authors

JEBÁČEK, I.

RIV year

2011

Released

19.09.2010

Publisher

Optimage Ltd.

Location

Edinburg, UK

ISBN

978-0-9565333-0-2

Book

27th Congress of International Council of Aeronautical Sciences

Edition

ICAS2010

Pages from

1

Pages to

7

Pages count

7

BibTex

@inproceedings{BUT36140,
  author="Ivo {Jebáček}",
  title="MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST",
  booktitle="27th Congress of International Council of Aeronautical Sciences",
  year="2010",
  series="ICAS2010",
  pages="1--7",
  publisher="Optimage Ltd.",
  address="Edinburg, UK",
  isbn="978-0-9565333-0-2"
}