Publication detail
The Sailplane Cockpit Structure during Emergency Landing Condition
MALIŠ, M. ŠPLÍCHAL, J.
English title
The Sailplane Cockpit Structure during Emergency Landing Condition
Type
Paper in proceedings (conference paper)
Language
en
Original abstract
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.
Keywords in English
crashworthiness, glider cocpit, finite elements methods simulation
Released
2006-09-03
Publisher
Optimage Ltd., Edinburgh, UK
Location
HAMBURG, GERMANY
ISBN
0-9533991-7-6
Book
CD PROCEEDINGS
Pages from–to
1–7
Pages count
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"
}