Investigation of maximum lift obtainable with slotted airfoils derived from symmetrical airfoil; center of lift travels contrary to usual direction as angle of attack is increased; tests of series of slotted airfoils derived from dissymmetrical airfoil. Translated from Service Technique de L'Aerotechnique Belge -- Bul., nos. 1 and 4, Apr. and July, 1927.
Results of aerodynamic tests on slotted airfoils in the aerotechnical laboratory (S. T. Ae.) of Rhone St. Genese, Brussels
Nat. Advisory Committee Aeronautics -- Tech. Memorandums
1928
19 pages
6 Figs.
Report
Englisch
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