Publication detail

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

AUGUSTIN, P. PLHAL, M. ŠPLÍCHAL, J.

English title

Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear

Type

Peer-reviewed article not indexed in WoS or Scopus

Language

en

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 in English

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

Released

2006-12-01

Publisher

VZLÚ, a.s.

ISSN

1211-877X

Journal

Letecký zpravodaj

Volume

2006

Number

3

Pages from–to

34–36

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"
}