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.
The Analysis of Aircraft Structures as Space Frameworks. Method Based on the Forces in the Longitudinal Members
1929-07-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1929
|Static and dynamic analysis of space frameworks with curved members
Tema Archive | 1979
|Stress analysis of aircraft frameworks
Engineering Index Backfile | 1941
|Electromagnetic forces on space structures
TIBKAT | 1966
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