Optimum stiffness inflated mattress beams

Simple item page
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

Files

Original bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
COA_Memo_204_September_1969.pdf
Size:
776.76 KB
Format:
Adobe Portable Document Format
Download

License bundle

Now showing 1 - 1 of 1
Thumbnail Image
Name:
license.txt
Size:
1.79 KB
Format:
Item-specific license agreed upon to submission
Description:
Download

Collections

CoA. Memoranda