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.


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    Title :

    The Analysis of Aircraft Structures as Space Frameworks. Method Based on the Forces in the Longitudinal Members


    Contributors:

    Publication date :

    1929-07-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





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