Publication detail

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

AUGUSTIN, P., PLHAL, M., ŠPLÍCHAL, J.

Original Title

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

Type

journal article - other

Language

English

Original Abstract

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.

Keywords

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

Authors

AUGUSTIN, P., PLHAL, M., ŠPLÍCHAL, J.

RIV year

2006

Released

1. 12. 2006

Publisher

VZLÚ, a.s.

ISBN

1211-877X

Periodical

Letecký zpravodaj

Year of study

2006

Number

3

State

Czech Republic

Pages from

34

Pages to

36

Pages count

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"
}