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    Wind-Tunnel and Flight Tests of Slot-lip Ailerons (1937)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: 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.
    Type: NACA-TR-602
    Format: application/pdf
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