On the natural frequencies of a reinforced circular cylinder

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dc.creator Hemp, W. S.
dc.date 2012-05-14T15:46:56Z
dc.date 2012-05-14T15:46:56Z
dc.date 1949-03
dc.date.accessioned 2022-05-09T10:17:17Z
dc.date.available 2022-05-09T10:17:17Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/7149
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4703
dc.description This report is concerned with the calculations of the natural frequencies of an ideal structure somewhat representative of an aircraft fuselage. The results are based upon a simplified “shell” theory which permits proper allowance to be made for the shear stresses and the corresponding displacements. No use is made of the so-called “shear deflection”, but it is shown in the Appendix that, for the special case considered, this approach would yield the same answer. Numerical results are given in x7 and comparison is made with both the usual beam theory results and the frequencies calculated on the assumption that flexibility in shear is of primary importance.
dc.language en
dc.publisher College of Aeronautics, Cranfield
dc.relation College Report
dc.relation 26
dc.title On the natural frequencies of a reinforced circular cylinder
dc.type Report

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