Publication detail
MEASUREMENT OF THE STRAIN AND BENDING MOMENT ON THE WING OF AN AIRCRAFT AND USING OF THESE FINDINGS FOR FATIGUE TEST
JEBÁČEK, I.
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)
Language
en
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.
Keywords in English
test, in flight, measurement, bending moment, fatigue
Released
2010-09-19
Publisher
Optimage Ltd.
Location
Edinburg, UK
ISBN
978-0-9565333-0-2
Book
27th Congress of International Council of Aeronautical Sciences
Pages from–to
1–7
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"
}