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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    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





    Determination of airplane critical altitude by flight tests

    Miller, L.C. | Engineering Index Backfile | 1942


    Airplane research work through flight tests

    Engineering Index Backfile | 1923



    Theoretical and Experimental Determination of Flight Performances of an Airplane in Martian Atmospheric Flight

    Teofilatto, P. / American Institute of Aeronautics and Astronautics / International Council of Aeronautical Sciences | British Library Conference Proceedings | 1996