Detail publikace
The Sailplane Cockpit Structure during Emergency Landing Condition
MALIŠ, M. ŠPLÍCHAL, J.
Anglický název
The Sailplane Cockpit Structure during Emergency Landing Condition
Typ
Stať ve sborníku v databázi WoS či Scopus
Jazyk
en
Originální abstrakt
The article describes the compliance evaluation of the glider cockpit crashworthiness numerical simulations with the static test. The design of the test and the numerical simulation model were prepared in accordance with JAR 22.561(b)(2) requirements. The next part demonstrates suggestion of crashworthiness methodology evaluation of glider cockpit with help pilot injuries criteria. The whole simulation was developed using the nonlinear explicit transient dynamic computer code MSC. Dytran. The test and the simulations were carried out by the Institute of Aerospace Engineering, Brno University of Technology.
Klíčová slova anglicky
crashworthiness, glider cocpit, finite elements methods simulation
Vydáno
2006-09-03
Nakladatel
Optimage Ltd., Edinburgh, UK
Místo
HAMBURG, GERMANY
ISBN
0-9533991-7-6
Kniha
CD PROCEEDINGS
Strany od–do
1–7
Počet stran
7
BIBTEX
@inproceedings{BUT20233,
author="Michal {Mališ} and Jan {Šplíchal}",
title="The Sailplane Cockpit Structure during Emergency Landing Condition",
booktitle="CD PROCEEDINGS",
year="2006",
pages="1--7",
publisher="Optimage Ltd., Edinburgh, UK",
address="HAMBURG, GERMANY",
isbn="0-9533991-7-6"
}