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Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 24
"This note is the fifth of a series covering an investigation of a number of related airfoils. It presents the results obtained from tests of a group of six low-cambered airfoils in the variable-density wind tunnel. The mean camber lines are identical for the six airfoils and are of such a form that the maximum mean camber is 2 per cent of the chord and is at a position 0.4 of the chord behind the loading edge. The airfoils differ in thickness only, the maximum-thickness/chord ratios being 0.06, 0.09, 0.12, 0.15, 0.18, and 0.21" (p. 1).
Date:
January 1932
Creator:
Jacobs, Eastman N. & Ward, Kenneth E.
System:
The UNT Digital Library