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| Published in: | Fatigue of Aircraft Structures |
|---|---|
| Format: | Online Article RSS Article |
| Published: |
2025
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| Subjects: | |
| Tags: |
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| _version_ | 1864030189027065856 |
|---|---|
| collection | WordPress RSS FRELIP Feed Integration |
| container_title | Fatigue of Aircraft Structures |
| description | |
| discipline_display | Engineering & Technology |
| discipline_facet | Engineering & Technology |
| format | Online Article RSS Article |
| genre | Journal Article |
| id | rss_article:12029 |
| institution | FRELIP |
| journal_source_facet | Fatigue of Aircraft Structures |
| publishDate | 2025 |
| publishDateSort | 2025 |
| record_format | rss_article |
| spellingShingle | Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model Aeronautics and space flight Aerospace & Aeronautical Engineering & Technology |
| sub_discipline_display | Aerospace & Aeronautical |
| sub_discipline_facet | Aerospace & Aeronautical |
| subject_display | Aeronautics and space flight Aerospace & Aeronautical Engineering & Technology Aeronautics and space flight Aerospace & Aeronautical Engineering & Technology |
| subject_facet | Aeronautics and space flight Aerospace & Aeronautical Engineering & Technology |
| title | Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model |
| title_auth | Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model |
| title_full | Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model |
| title_fullStr | Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model |
| title_full_unstemmed | Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model |
| title_short | Residual Strength Analysis of a Composite Stiffened Panel After a Stiffener Debonding Using an Industrial Numerical Damage Model |
| title_sort | residual strength analysis of a composite stiffened panel after a stiffener debonding using an industrial numerical damage model |
| topic | Aeronautics and space flight Aerospace & Aeronautical Engineering & Technology |
| url | https://sciendo.com/article/10.2478/fas-2024-0004 |