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Formulation of a new finite element based on assumed strains for membrane structures

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Bibliographic Details
Published in:International Journal of Advanced Structural Engineering
Format: Online Article RSS Article
Published: 2019
Subjects:
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container_title International Journal of Advanced Structural Engineering
description
discipline_display Technology & Engineering
discipline_facet Technology & Engineering
format Online Article
RSS Article
genre Journal Article
id rss_article:32917
institution FRELIP
journal_source_facet International Journal of Advanced Structural Engineering
publishDate 2019
publishDateSort 2019
record_format rss_article
spellingShingle Formulation of a new finite element based on assumed strains for membrane structures
Building and Construction
Technology & Engineering — Aerospace & Applied Tech
Technology & Engineering
sub_discipline_display Technology & Engineering — Aerospace & Applied Tech
sub_discipline_facet Technology & Engineering — Aerospace & Applied Tech
subject_display Building and Construction
Technology & Engineering — Aerospace & Applied Tech
Technology & Engineering
Building and Construction
Technology & Engineering — Aerospace & Applied Tech
Technology & Engineering
subject_facet Building and Construction
Technology & Engineering — Aerospace & Applied Tech
Technology & Engineering
title Formulation of a new finite element based on assumed strains for membrane structures
title_auth Formulation of a new finite element based on assumed strains for membrane structures
title_full Formulation of a new finite element based on assumed strains for membrane structures
title_fullStr Formulation of a new finite element based on assumed strains for membrane structures
title_full_unstemmed Formulation of a new finite element based on assumed strains for membrane structures
title_short Formulation of a new finite element based on assumed strains for membrane structures
title_sort formulation of a new finite element based on assumed strains for membrane structures
topic Building and Construction
Technology & Engineering — Aerospace & Applied Tech
Technology & Engineering
url https://link.springer.com/article/10.1007/s40091-019-00251-9