Optimum stiffness inflated mattress beams

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dc.contributor.authorWebb, J.
dc.date.accessioned2016-04-15T13:24:08Z
dc.date.available2016-04-15T13:24:08Z
dc.date.issued1969-09
dc.description.abstractThis 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.en_UK
dc.identifier.urihttp://dspace.lib.cranfield.ac.uk/handle/1826/9819
dc.language.isoenen_UK
dc.publisherCollege of Aeronauticsen_UK
dc.relation.ispartofseriesCoA/M-204en_UK
dc.relation.ispartofseries202en_UK
dc.titleOptimum stiffness inflated mattress beamsen_UK
dc.typeReporten_UK

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