FE-Modelling Methodology of Riveted Joints

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F16361733%3A_____%2F10%3A%230000010" target="_blank" >RIV/16361733:_____/10:#0000010 - isvavai.cz</a>
Result on the web
<a href="http://www.czaerospace.eu/en/2010-02-35.html" target="_blank" >http://www.czaerospace.eu/en/2010-02-35.html</a>
DOI - Digital Object Identifier
—

Result language
angličtina
Original language name
FE-Modelling Methodology of Riveted Joints
Original language description
Riveting is the most common way of connecting parts together in the aircraft industry. This document deals with finite element (FE) simulations of riveted joints of various complexity. The riveted structures are modelled realistically including first thephase of forming a riveted joint and then also the shearing of the joint. Some parameters influencing behaviour of such joints are evaluated in further FE-analyses. Properly tuned detailed solid FE-models were then used for a definition of their suitable replacement by simpler modelling structures. The replacement allows engineering application of rivets to more complex loads of aircraft structures while keeping the computation time acceptably short.
Czech name
—
Czech description
—

Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JU - Aeronautics, aerodynamics, aeroplanes
OECD FORD branch
—

Project
<a href="/en/project/OE08006" target="_blank" >OE08006: Improving the Fatigue Performance of Riveted Joints in Airframes</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2010
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Similar results(10)