Publication detail
THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION
JURAČKA, J. MALIŠ, M.
English title
THE COMPOSITE COCKPIT STRUCTURE BEHAVIOR DURING EMERGENCY LANDING CONDITION
Type
Paper in proceedings (conference paper)
Language
en
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 in English
aviation, aircraft, composite structure
Released
2006-09-29
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–to
99–
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"
}