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Communication Dans Un Congrès Année : 2009

Numerical computation of the deployment of a folded inflatable tube

Résumé

This work deals with the numerical simulation of the deployment of a folded inflatable structure subjected to an internal pressure. The computation is performed by means of the finite element method as opposed to most of other works which used the control volume method. During the deployment process, self contact can occur at some portions of the boundary where contact force play a crucial role to deploy the structure. Contact problem will be treated by making use of a new weighted residual principle.
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Dates et versions

hal-04621269 , version 1 (23-06-2024)

Identifiants

  • HAL Id : hal-04621269 , version 1

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Nguyen Huynh Tan Tai, Anh Le Van. Numerical computation of the deployment of a folded inflatable tube. IV International Conference on Textile Composites and Inflatable Structures, 2009, Barcelone, Spain. ⟨hal-04621269⟩
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