Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite Panels
This paper aims to study the dynamic behaviors of particular sandwich panels manufactured using three specifications of aluminum honeycomb core with fiberglass or aluminum face-sheet materials. Three groups of panels were designed and manufactured, each including three different sorts of samples, a...
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| Format: | Article |
| Language: | English |
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Tikrit University
2023-07-01
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| Series: | Tikrit Journal of Engineering Sciences |
| Subjects: | |
| Online Access: | https://tj-es.com/ojs/index.php/tjes/article/view/1039 |
| _version_ | 1797754555102920704 |
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| author | Ahmed Ali Khalid Fadhel Abbas Abdulla Mushtaq Al-Sharify |
| author_facet | Ahmed Ali Khalid Fadhel Abbas Abdulla Mushtaq Al-Sharify |
| author_sort | Ahmed Ali Khalid |
| collection | DOAJ |
| description |
This paper aims to study the dynamic behaviors of particular sandwich panels manufactured using three specifications of aluminum honeycomb core with fiberglass or aluminum face-sheet materials. Three groups of panels were designed and manufactured, each including three different sorts of samples, all fabricated with the same thickness. A cantilever fatigue test was conducted on specimens, and the results were collected and presented in curves to detect the factors that affect the panel's endurance. The finding showed that the specimens with aluminum skin had more probability of face-sheet/core delamination. Samples of fiberglass covers showed face-sheets cracks or cores cracks more than delamination failure, while samples of epoxy-filled cores experienced the specimen’s global crack. Generally, specimens with aluminum covers and epoxy-filled cores resisted fatigue load more than other specimens. The larger honeycomb cell-size specimens showed more probability to face-sheet/core delamination failures than samples with smaller cell-size cores.
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| first_indexed | 2024-03-12T17:34:10Z |
| format | Article |
| id | doaj.art-f00e196a09b74ac48f831d69f8e07103 |
| institution | Directory Open Access Journal |
| issn | 1813-162X 2312-7589 |
| language | English |
| last_indexed | 2024-03-12T17:34:10Z |
| publishDate | 2023-07-01 |
| publisher | Tikrit University |
| record_format | Article |
| series | Tikrit Journal of Engineering Sciences |
| spelling | doaj.art-f00e196a09b74ac48f831d69f8e071032023-08-04T13:10:08ZengTikrit UniversityTikrit Journal of Engineering Sciences1813-162X2312-75892023-07-0130210.25130/tjes.30.2.13Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite PanelsAhmed Ali Khalid 0Fadhel Abbas Abdulla 1Mushtaq Al-Sharify2Mechanical Department/ Engineering College/Mustansiriyah University /Baghdad, IraqMechanical Department/ Engineering College/Mustansiriyah University /Baghdad, IraqRadio Engineering and Radio Electronics Systems Department / Radiophysics, Electronics, and Computer Systems Faculty, Taras Shevchenko National University of Kyiv / Kyiv, Ukraine. This paper aims to study the dynamic behaviors of particular sandwich panels manufactured using three specifications of aluminum honeycomb core with fiberglass or aluminum face-sheet materials. Three groups of panels were designed and manufactured, each including three different sorts of samples, all fabricated with the same thickness. A cantilever fatigue test was conducted on specimens, and the results were collected and presented in curves to detect the factors that affect the panel's endurance. The finding showed that the specimens with aluminum skin had more probability of face-sheet/core delamination. Samples of fiberglass covers showed face-sheets cracks or cores cracks more than delamination failure, while samples of epoxy-filled cores experienced the specimen’s global crack. Generally, specimens with aluminum covers and epoxy-filled cores resisted fatigue load more than other specimens. The larger honeycomb cell-size specimens showed more probability to face-sheet/core delamination failures than samples with smaller cell-size cores. https://tj-es.com/ojs/index.php/tjes/article/view/1039Composite panelshoneycombface sheetCoreFatigue |
| spellingShingle | Ahmed Ali Khalid Fadhel Abbas Abdulla Mushtaq Al-Sharify Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite Panels Tikrit Journal of Engineering Sciences Composite panels honeycomb face sheet Core Fatigue |
| title | Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite Panels |
| title_full | Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite Panels |
| title_fullStr | Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite Panels |
| title_full_unstemmed | Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite Panels |
| title_short | Experimental Investigation on the Fatigue Behavior on Honeycomb Sandwich Composite Panels |
| title_sort | experimental investigation on the fatigue behavior on honeycomb sandwich composite panels |
| topic | Composite panels honeycomb face sheet Core Fatigue |
| url | https://tj-es.com/ojs/index.php/tjes/article/view/1039 |
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