Detail publikace

THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION

JURAČKA, J. MALIŠ, M.

Originální název

THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION

Typ

článek ve sborníku ve WoS nebo Scopus

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

aviation, aircraft, composite structure

Autoři

JURAČKA, J.; MALIŠ, M.

Rok RIV

2006

Vydáno

29. 9. 2006

Nakladatel

University of Žilina

Místo

Žilina, Slovak Rep.

ISBN

80-8070-589-5

Kniha

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

Strany od

99

Strany do

100

Strany počet

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"
}