Detail publikace
Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear
AUGUSTIN, P. PLHAL, M. ŠPLÍCHAL, J.
Anglický název
Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear
Typ
Článek recenzovaný mimo WoS a Scopus
Jazyk
en
Originální abstrakt
The paper deals with the fatigue evaluation of the VUT100 Cobra airplane landing gear. Institute of Aerospace Engineering BUT participates in the solution of this problem with fatigue calculation based on the results of FEM stress analysis. IAE also provides generation of load sequence and data for the control electronic of servohydraulic testing system for fatigue tests performed at the laboratory of the landing gear producer Technometra Radotin Plc. The fatigue tests of both main and nose landing gears are currently carrying out. Their results allow verification of fatigue analyses and improvement of their methodology.
Klíčová slova anglicky
aircraft landing gear, fatigue testing, load sequence, fatigue analysis, FEM
Vydáno
2006-12-01
Nakladatel
VZLÚ, a.s.
ISSN
1211-877X
Časopis
Letecký zpravodaj
Ročník
2006
Číslo
3
Strany od–do
34–36
Počet stran
3
BIBTEX
@article{BUT44215,
author="Petr {Augustin} and Martin {Plhal} and Jan {Šplíchal}",
title="Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear",
journal="Letecký zpravodaj",
year="2006",
volume="2006",
number="3",
pages="34--36",
issn="1211-877X"
}