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Damage evaluation based on ultrasonic testing of compos-ite aircraft elements and image analysis met...

Damage evaluation based on ultrasonic testing of compos-ite aircraft elements and image analysis met...

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_fc5d7cd5466d41549ab41d7c43637a70

Damage evaluation based on ultrasonic testing of compos-ite aircraft elements and image analysis methods

About this item

Full title

Damage evaluation based on ultrasonic testing of compos-ite aircraft elements and image analysis methods

Publisher

Les Ulis: EDP Sciences

Journal title

MATEC web of conferences, 2018-01, Vol.204, p.6003

Language

English

Formats

Publication information

Publisher

Les Ulis: EDP Sciences

More information

Scope and Contents

Contents

Composite aircraft elements are inspected with the use of non-destructive testing methods to detect the damage appearance and monitor its progression. Ultrasonic testing is one of the most commonly applied methods owing to its capabilities of detecting various types of internal flaws and dam-age as well as evaluating their location and geometrical...

Alternative Titles

Full title

Damage evaluation based on ultrasonic testing of compos-ite aircraft elements and image analysis methods

Authors, Artists and Contributors

Identifiers

Primary Identifiers

Record Identifier

TN_cdi_doaj_primary_oai_doaj_org_article_fc5d7cd5466d41549ab41d7c43637a70

Permalink

https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_fc5d7cd5466d41549ab41d7c43637a70

Other Identifiers

ISSN

2261-236X,2274-7214

E-ISSN

2261-236X

DOI

10.1051/matecconf/201820406003

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