Derivation of empirical equation to fit experimental values of profile drag determined from N A C A tests on uniform-section rectangular airfoils at varying lift coefficients; determining profile drag of more general airfoil; induced drag is simplified and combined with profile drag to get complete expression for drag coefficient of tapered airfoil; relative merit of various planeforms.
Drag of tapered cantilever airfoils
Aeronautical Sciences -- J
Journal of Aeronautical Sciences ; 1 , n 4
1934
10 pages
Article (Journal)
English
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