Thermo-viscoelastic modeling of the aircraft tire cornering - Archive ouverte HAL Access content directly
Journal Articles Advanced Materials Research Year : 2015

Thermo-viscoelastic modeling of the aircraft tire cornering

Abstract

Some numerical models are proposed for simulate the aircraft tire behaviour on the ground in critical situations. Fully coupled thermo-mechanical analysis procedures taking into account finite deformation, dynamics and frictional contact are studied; the visco-elasticity properties of the rubber were identified. A good agreement is observed at moderate speed, thus the model is extrapolated to high speeds and seems able to predict results in cases for which it is not possible to obtain realistic experimental data. In order to understand the thermal evolution of tire tread rubber materials during rolling and skidding steps, new experimental and numerical studies were also realized on tire tread rubber. The aim of this approach is to simulate and understand the effect of frictional heating on the tire behaviour.
Fichier principal
Vignette du fichier
2015-rosu-et-al.pdf (392.52 Ko) Télécharger le fichier
Origin Files produced by the author(s)

Dates and versions

hal-01247910 , version 1 (04-06-2018)

Identifiers

Cite

Iulian Rosu, Hélène Elias-Birembaux, Frédéric Lebon. Thermo-viscoelastic modeling of the aircraft tire cornering. Advanced Materials Research, 2015, 1099, pp.80-86. ⟨10.4028/www.scientific.net/AMR.1099.80⟩. ⟨hal-01247910⟩

Relations

69 View
102 Download

Altmetric

Share

Gmail Mastodon Facebook X LinkedIn More