The Analysis of Aircraft Structures as Space Frameworks: Method Based on the Forces in the Longitudinal Members
Description:
The following examples do not take up the discussion of viewpoints to be heeded in determining the design of a framework for given external conditions. Rather they are methods for determining the forces in airplane fuselages and wings, though similar considerations are applied to certain simple cases of a different kind. The object of this treatise is to summarize and amplify these considerations from definite viewpoints.
Date:
July 1929
Creator:
Wagner, Herbert
Item Type:
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Partner:
UNT Libraries Government Documents Department