Detail publikace

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

AUGUSTIN, P., PLHAL, M., ŠPLÍCHAL, J.

Originální název

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

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

aircraft landing gear, fatigue testing, load sequence, fatigue analysis, FEM

Autoři

AUGUSTIN, P., PLHAL, M., ŠPLÍCHAL, J.

Rok RIV

2006

Vydáno

1. 12. 2006

Nakladatel

VZLÚ, a.s.

ISSN

1211-877X

Periodikum

Letecký zpravodaj

Ročník

2006

Číslo

3

Stát

Česká republika

Strany od

34

Strany do

36

Strany počet

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"
}