Tests of large airfoils in the propeller research tunnel, including two with corrugated surfaces

Wood, Donald H
naca-report-336
1930


This report gives the results of the tests of seven 2 by 12 foot airfoils (Clark Y, smooth and corrugated, Gottingen 398, N.A.C.A. M-6, and N.A.C.A. 84). The tests were made in the propeller research tunnel of the National Advisory Committee for Aeronautics at Reynolds numbers up to 2,000,000. The Clark Y airfoil was tested with three degrees of surface smoothness. Corrugating the surface causes a flattening of the lift curve at the burble point and an increase in drag at small flying angles.

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http://naca.central.cranfield.ac.uk/reports/1930/naca-report-336.pdf