Response of thin-walled cylinders to aerodynamic excitation
Non-linear vibrations of thin-walled shells under aerodynamic excitation are investigated using Flugge's thin-shell theory, modified to include the effects of large deformations. The theory is applicable to any type of boundary conditions and various types of normal loading. The formulation inc...
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Loughborough University
1974
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| Online Access: | https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.466860 |