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AUGUSTIN, P., PLHAL, M., ŠPLÍCHAL, J.
Original Title
Fatigue Testing and Analysis of VUT 100 Aircraft Landing Gear
English Title
Type
Peer-reviewed article not indexed in WoS or Scopus
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.
English abstract
Keywords
aircraft landing gear, fatigue testing, load sequence, fatigue analysis, FEM
Key words in English
Authors
Released
01.12.2006
Publisher
VZLÚ, a.s.
ISBN
1211-877X
Periodical
Letecký zpravodaj
Volume
2006
Number
3
State
Czech Republic
Pages from
34
Pages to
36
Pages count
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" }