| 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 |
| Files | Size | Format | View |
|---|---|---|---|
| COA_Memo_204_September_1969.pdf | 795.4Kb | application/pdf |
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