Publication detail

Static analysis of VUT100 Aircraft Main and Nose-wheel Landing Gear

PLHAL, M.

Original Title

Static analysis of VUT100 Aircraft Main and Nose-wheel Landing Gear

Type

journal article - other

Language

English

Original Abstract

The paper provides description of FEM stress analysis of landing gears for new aircraft VUT100. In all loading cases, there is considered material and geometric non-linearity, contacts and friction between some parts of landing gear. The certification processes require the structural testing of all parts. It means that each modification should be verified by a test. The FAR 23 and JAR 23 regulations provide the possibility to certify the aircraft components, landing gear inclusive, without verification by structural test under condition that the employed analysis was proved reliable in the past for very similar component.

Keywords

Landing Gear, Analysis

Authors

PLHAL, M.

Released

21. 11. 2003

ISBN

1211-877X

Periodical

Letecký zpravodaj

Year of study

2003

Number

3

State

Czech Republic

Pages from

9

Pages to

11

Pages count

3

BibTex

@article{BUT41957,
  author="Martin {Plhal}",
  title="Static analysis of VUT100 Aircraft Main and Nose-wheel Landing Gear",
  journal="Letecký zpravodaj",
  year="2003",
  volume="2003",
  number="3",
  pages="3",
  issn="1211-877X"
}