Detail publikace

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

PLHAL, M.

Originální název

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

Typ

článek v časopise - ostatní, Jost

Jazyk

angličtina

Originální abstrakt

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.

Klíčová slova

Landing Gear, Analysis

Autoři

PLHAL, M.

Vydáno

21. 11. 2003

ISSN

1211-877X

Periodikum

Letecký zpravodaj

Ročník

2003

Číslo

3

Stát

Česká republika

Strany od

9

Strany do

11

Strany počet

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"
}