It has been demonstrated that maneuvering loads due to motions about all three axes of airplane can be readily determined analytically for sequence of control movement varying linearly with time up to specified value and then held constant; it will be found that, in general, linear sequence is most adaptable to limitations such as set up in maneuvering horizontal tail load problem.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Airplane maneuvering loads


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1946


    Size :

    7 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English