Publication detail

THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION

JURAČKA, J. MALIŠ, M.

Original Title

THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION

Type

conference paper

Language

English

Original Abstract

Increasing possibilities of simulation cause enhancement of the safety requirements in aerospace engineering. The trend did not avoid glider cockpit structures too. The investigation of a cockpit resistance during the emergency landing condition is always an important area of interest. In former times the cockpit design was the result of experience and tests. Now, there are a several finite element methods (FEM) systems for simulation of emergency landing condition.

Keywords

aviation, aircraft, composite structure

Authors

JURAČKA, J.; MALIŠ, M.

RIV year

2006

Released

29. 9. 2006

Publisher

University of Žilina

Location

Žilina, Slovak Rep.

ISBN

80-8070-589-5

Book

23rd DANUBIA-ADRIA Sympozium on Experimental methods in Solid Mechanic

Pages from

99

Pages to

100

Pages count

2

BibTex

@inproceedings{BUT19685,
  author="Jaroslav {Juračka} and Michal {Mališ}",
  title="THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION",
  booktitle="23rd DANUBIA-ADRIA Sympozium on Experimental methods in Solid Mechanic",
  year="2006",
  pages="2",
  publisher="University of Žilina",
  address="Žilina, Slovak Rep.",
  isbn="80-8070-589-5"
}