Compounded normal modes of free vibration of cantilever plates

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dc.contributor.authorKirk, Colin L.
dc.date.accessioned2017-07-31T08:24:13Z
dc.date.available2017-07-31T08:24:13Z
dc.date.issued1967-04
dc.description.abstractExperimental determination of the natural frequencies of a stiffened cantilever plate reveals the simultaneous excitation of two normal modes of vibration. Comparison is made between the experimental nodal pattern and the nodal pattern calculated by assuming characteristic beam functions for the vibration form of the plate.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/12247
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/N/AERO-173en_UK
dc.relation.ispartofseries173en_UK
dc.titleCompounded normal modes of free vibration of cantilever platesen_UK
dc.typeReporten_UK

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CoA. Aero Notes (1963-1975)