Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight

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dc.creator Howe, D.
dc.date 2012-09-13T15:27:37Z
dc.date 2012-09-13T15:27:37Z
dc.date 1953-08
dc.date.accessioned 2022-05-09T10:17:21Z
dc.date.available 2022-05-09T10:17:21Z
dc.identifier http://dspace.lib.cranfield.ac.uk/handle/1826/7578
dc.identifier.uri https://reports.aerade.cranfield.ac.uk/handle/1826.2/4751
dc.description The specimen used in this work represents the load carrying structure of a cambered two spar 60 degree sweptback wing, having closely pitched ribs of large boom area parallel to the line of flight, and thick skins. Continues …
dc.language en
dc.publisher College of Aeronautics, Cranfield
dc.relation College Reports
dc.relation 66
dc.title Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight
dc.type Report


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