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Wind-Tunnel and Flight Tests of Slot-lip AileronsThe 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.
Document ID
19930091678
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Shortal, Joseph A
Date Acquired
September 6, 2013
Publication Date
January 1, 1937
Report/Patent Number
NACA-TR-602
Accession Number
93R20968
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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