Calculation of stresses in multi-spar stressed skin wings with strain gages; stress transfer between wing and fuselage also studied; strains due to oscillation of airplane tail in flight.


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    Title :

    Applications of electric strain gage in solution of aircraft structural design problems


    Additional title:

    Automotive Aviation Industries


    Published in:

    Publication date :

    1942


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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