Log in to save to my catalogue

Reliability analysis of composite sandwich structure for fuselage skin based on surrogate model

Reliability analysis of composite sandwich structure for fuselage skin based on surrogate model

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_3c82aa3859c44d86a16a577a3b5743ed

Reliability analysis of composite sandwich structure for fuselage skin based on surrogate model

About this item

Full title

Reliability analysis of composite sandwich structure for fuselage skin based on surrogate model

Publisher

EDP Sciences

Journal title

Xibei Gongye Daxue Xuebao, 2022-04, Vol.40 (2), p.360-368

Language

Formats

Publication information

Publisher

EDP Sciences

More information

Scope and Contents

Contents

Composite structures are characterized by multiple source uncertainties in mechanical properties, geometric dimension, etc., and multiple failure modes, which bring challenges to their design and application. In order to explore the reliability analysis method of composite sandwich structures with multi-source uncertainties and multi-failure modes,...

Alternative Titles

Full title

Reliability analysis of composite sandwich structure for fuselage skin based on surrogate model

Authors, Artists and Contributors

Identifiers

Primary Identifiers

Record Identifier

TN_cdi_doaj_primary_oai_doaj_org_article_3c82aa3859c44d86a16a577a3b5743ed

Permalink

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_3c82aa3859c44d86a16a577a3b5743ed

Other Identifiers

ISSN

1000-2758

E-ISSN

2609-7125

DOI

10.1051/jnwpu/20224020360

How to access this item