cris.boxmetadata.label.title
High-fidelity simulations of thin shell deployable structures with adaptive meshing
cris.boxmetadata.label.dateissued
01 browse.startsWith.months.january 2022
cris.boxmetadata.label.accesslevel
metadata only access
cris.boxmetadata.label.resourcetype
conference paper
cris.boxmetadata.label.authors
Pellegrino S.
California Institute of Technology
cris.boxmetadata.label.publisher
American Institute of Aeronautics and Astronautics
cris.boxmetadata.label.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.
cris.boxmetadata.label.language
English
cris.boxmetadata.label.ocdeknowledgeArea
Ingeniería aeroespacial
cris.boxmetadata.label.doi
cris.boxmetadata.label.scopusidentifier
2-s2.0-85123578046
cris.boxmetadata.label.containerisbn
978-162410631-6
cris.boxmetadata.label.conference
AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
peru-layout.shadow-copies
Directorio de Producción Científica
Scopus