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Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading

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Published in:Fatigue of Aircraft Structures
Format: Online Article RSS Article
Published: 2025
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container_title Fatigue of Aircraft Structures
description
discipline_display Aeronautics and space flight
discipline_facet Aeronautics and space flight
format Online Article
RSS Article
genre Journal Article
id rss_article:85043
institution FRELIP
journal_source_facet Fatigue of Aircraft Structures
publishDate 2025
publishDateSort 2025
record_format rss_article
spellingShingle Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading
Aeronautics and space flight
General
Aeronautics and space flight
sub_discipline_display General
sub_discipline_facet General
subject_display Aeronautics and space flight
General
Aeronautics and space flight
Aeronautics and space flight
General
Aeronautics and space flight
subject_facet Aeronautics and space flight
General
Aeronautics and space flight
title Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading
title_auth Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading
title_full Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading
title_fullStr Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading
title_full_unstemmed Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading
title_short Experimental Investigation and Failure Criterion Development for CFR Composite Tubular Specimens Under Combined Axial and Pressure Loading
title_sort experimental investigation and failure criterion development for cfr composite tubular specimens under combined axial and pressure loading
topic Aeronautics and space flight
General
Aeronautics and space flight
url https://sciendo.com/article/10.2478/fas-2025-0003