Detail publikace

The Sailplane Cockpit Structure during Emergency Landing Condition

MALIŠ, M. ŠPLÍCHAL, J.

Originální název

The Sailplane Cockpit Structure during Emergency Landing Condition

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

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

crashworthiness, glider cocpit, finite elements methods simulation

Autoři

MALIŠ, M.; ŠPLÍCHAL, J.

Rok RIV

2006

Vydáno

3. 9. 2006

Nakladatel

Optimage Ltd., Edinburgh, UK

Místo

HAMBURG, GERMANY

ISBN

0-9533991-7-6

Kniha

CD PROCEEDINGS

Strany od

1

Strany do

7

Strany počet

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"
}