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|Document Type: ||Report|
|Title: ||Testing and analysis of a 60 degrees swept back wing with ribs parallel to the line of flight|
|Authors: ||Howe, D.|
|Issue Date: ||Aug-1953|
|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 …|
|Appears in Collections:||College of Aeronautics Reports|
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