The slot-lip ailerons developed by the NACA consist of a flap-type spoiler with an adjoining continuously open slot. The ailerons were developed in an investigation of the delayed response, or lag, of spoiler-type lateral controls. This report presents the results of tests of these slot-lip ailerons made on wing models in the 7 by 10-foot wind tunnel, on a Fairchild 22 airplane in the full-scale wind tunnel and in flight, and on the Weick W1-A airplane in flight.


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    Titel :

    Wind-Tunnel and Flight Tests of Slot-lip Ailerons


    Beteiligte:

    Erscheinungsdatum :

    01.01.1937


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch



    Wind-tunnel and flight tests of slot-tip ailerons

    Shortal, J.A. | Engineering Index Backfile | 1937


    Wind-tunnel and flight tests of slot-tip ailerons

    Shortal, J.A. | Engineering Index Backfile | 1937


    Wind-tunnel and flight tests of slot-lip ailerons

    Shortal, Joseph A. | TIBKAT | 1937


    Wind-tunnel and flight tests of slot-tip ailerons

    Shortal, J.A. | Engineering Index Backfile | 1937


    Wind tunnel tests on Junker type ailerons

    Bradfield, F. B. ;Wood, W. E. | SLUB | 1934