Detail publikace

THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION

JURAČKA, J. MALIŠ, M.

Anglický název

THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION

Typ

Stať ve sborníku v databázi WoS či Scopus

Jazyk

en

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 anglicky

aviation, aircraft, composite structure

Vydáno

2006-09-29

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–do

99–

Počet stran

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"
}