FREE VIBRATION ANALYSIS OF COMPOSITE AIRCRAFT WING WITH CIRCULAR CUTOUT USING FINITE ELEMENT METHOD
In the present study, the effect of circular cutout in the skin of composite aircraft wing on the natural frequencies was studied by finite element method using ANSYS software version 11. The case which was studied is the presence of circular cutout in the skin of the wing through its thickness. Th...
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| Format: | Article |
| Language: | English |
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University of Diyala
2015-12-01
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| Series: | Diyala Journal of Engineering Sciences |
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| Online Access: | https://djes.info/index.php/djes/article/view/407 |