Detail publikačního výsledku

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

JEBÁČEK, I.

Originální název

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

Anglický název

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

Druh

Stať ve sborníku v databázi WoS či Scopus

Originální abstrakt

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.

Anglický abstrakt

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.

Klíčová slova

test, in flight, measurement, bending moment, fatigue

Klíčová slova v angličtině

test, in flight, measurement, bending moment, fatigue

Autoři

JEBÁČEK, I.

Rok RIV

2011

Vydáno

19.09.2010

Nakladatel

Optimage Ltd.

Místo

Edinburg, UK

ISBN

978-0-9565333-0-2

Kniha

27th Congress of International Council of Aeronautical Sciences

Edice

ICAS2010

Strany od

1

Strany do

7

Strany počet

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"
}