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Publication result detail
PLHAL, M.
Original Title
Static analysis of VUT100 Aircraft Main and Nose-wheel Landing Gear
English Title
Type
Peer-reviewed article not indexed in WoS or Scopus
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.
English abstract
Keywords
Landing Gear, Analysis
Key words in English
Authors
Released
21.11.2003
ISBN
1211-877X
Periodical
Letecký zpravodaj
Volume
2003
Number
3
State
Czech Republic
Pages from
9
Pages count
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" }