Thickening of optimally selected locations on panels subjected to unyawed flow for substantial delay of the panel flutter
In the current research, optimal locations on aircraft panels are thickened to delay the flutter occurrence. A standard square isotropic Aluminum panel of 12 × 12 in. is considered. In formulating the model, the Kirchhoff-Love hypothesis and the Von-Karman nonlinear strain-displacement relations are...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Elsevier
2020-12-01
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| Series: | Alexandria Engineering Journal |
| Subjects: | |
| Online Access: | http://www.sciencedirect.com/science/article/pii/S1110016820304828 |