Based on comparison between flight measurement results and calculations, data are obtained for sufficiently accurate calculation of resulting normal forces on wing truss structure and horizontal tail surface during accelerated longitudinal motion of elevator controlled airplane.


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    Title :

    Flight tests and calculations for determination of atmospheric forces on airplane with elevator action


    Additional title:

    Flugversuche und Rechnungen zur Bestimmung der Luftkraefte am Flugzeug, etc


    Contributors:
    Kaul, H.W. (author) / Lindemann, H. (author)


    Publication date :

    1938


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    German