Optimum stiffness inflated mattress beams

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dc.creator Webb, J.
dc.date 2016-04-15T13:24:08Z
dc.date 2016-04-15T13:24:08Z
dc.date 1969-09
dc.date.accessioned 2022-05-09T09:55:07Z
dc.date.available 2022-05-09T09:55:07Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/9819
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4302
dc.description This report considers primarily the relatively short cantilever type of inflated matresss beam, currently being employed as sidebody structure on some hovercraft. The rib pitch for optimum stiffness/weight of such beams is determined, and it is shown that thin ribs, closely pitched, with relatively thick skins provide the most efficient structures.
dc.language en
dc.publisher College of Aeronautics
dc.relation CoA/M-204
dc.relation 202
dc.title Optimum stiffness inflated mattress beams
dc.type Report

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