Title
High-fidelity simulations of thin shell deployable structures with adaptive meshing
Date Issued
01 January 2022
Access level
metadata only access
Resource Type
conference paper
Author(s)
California Institute of Technology
Publisher(s)
American Institute of Aeronautics and Astronautics
Abstract
An adaptive meshing procedure is developed for the analysis of thin shell structures that experience localized elastic deformations associated with the formation of folds. The refinement criterion for remeshing takes into consideration the localization of deformation in the folds, while avoiding excessive refinement outside this region. The local bending strains in two principal directions are used to construct the refinement criterion. A geometrical parameter related to a boundary layer effect is shown to be effective as a limit length for refinement. Isogeometric shell finite elements are used for the simulations. Different tape spring geometries are simulated to illustrate the generality and efficiency of the proposed adaptive procedure.
Language
English
OCDE Knowledge area
Ingeniería aeroespacial
Scopus EID
2-s2.0-85123578046
ISBN of the container
978-162410631-6
Conference
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Sources of information: Directorio de Producción Científica Scopus