Publication detail

The Sailplane Cockpit Structure during Emergency Landing Condition

MALIŠ, M. ŠPLÍCHAL, J.

Original Title

The Sailplane Cockpit Structure during Emergency Landing Condition

Type

conference paper

Language

English

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

crashworthiness, glider cocpit, finite elements methods simulation

Authors

MALIŠ, M.; ŠPLÍCHAL, J.

RIV year

2006

Released

3. 9. 2006

Publisher

Optimage Ltd., Edinburgh, UK

Location

HAMBURG, GERMANY

ISBN

0-9533991-7-6

Book

CD PROCEEDINGS

Pages from

1

Pages to

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"
}