Results of tests of wing sections characterized by small travel of the center of pressure, tested at 20-atmos pressure in variable-density wind tunnel of Nat. Advisory Committee for Aeronautics, giving consistent results and showing that for stable sections a small effective camber, a small effective S-shape and a thickness of 8 to 12 per cent, lead to good aerodynamic properties.
Model tests with a systematic series of 27 wing sections at full Reynolds number
U.S. Nat. AdvisoryComm. Aeronautics -- Report
1925
18 pages
27 Figs.
Report
Englisch
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The aerodynamic characteristics of seven frequently used wing sections at full Reynolds number
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