This report gives the results of a recent series of experiments performed on a wing designed for a cantilever monoplane. Both wings were trapezial in their ground plan, with their tips rounded elliptically. These wing sections combine all known devices for increasing the lift, namely, the slot, the increased camber and angle of attack by means of an aileron running the whole length of the span. The last advance included in the wing section was an increase in wing area by means of an auxiliary wing adjusted by a sort of rectangular joint.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Results of recent experiments with slotted wings


    Contributors:
    Lachmann, G (author)

    Publication date :

    1925-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English





    Experiments wit slotted wings

    Lachmann, G | NTRS | 1921


    Experimental results with slotted wings

    Lachmann, G. | Engineering Index Backfile | 1924


    Slotted wings

    Handley Page, F. | Engineering Index Backfile | 1928


    Airplanes with slotted wings

    Everling, E. | Engineering Index Backfile | 1927