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RAPID FLUTTER ANALYSIS FOR LOW-ASPECT-RATIO WINGS WITH A CONTROL SURFACE
An effective method and fast modeling in vibration and flutter analyses of low-aspect-ratio composite wings and wings with a control surface in a subsonic flow are proposed. An equivalent plate method is used for structural modeling. The doublet point and the methods are applied to calculate unstead...
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Published in: | Journal of applied mechanics and technical physics 2022-02, Vol.63 (1), p.59-66 |
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Main Authors: | , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites |
Online Access: | Get full text |
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Summary: | An effective method and fast modeling in vibration and flutter analyses of low-aspect-ratio composite wings and wings with a control surface in a subsonic flow are proposed. An equivalent plate method is used for structural modeling. The doublet point and the
methods are applied to calculate unsteady aerodynamic loads and flutter analysis, respectively. The obtained results are in good agreement with the literature data. |
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ISSN: | 0021-8944 1573-8620 |
DOI: | 10.1134/S0021894422010102 |