Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight
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Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight
Howe, D.
URI:
http://dspace.lib.cranfield.ac.uk/handle/1826/7578
Date:
1953-08
Abstract:
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 …
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CoA. Reports
[280]
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