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The Effect on Lift, Drag, and Spinning Characteristics of Sharp Leading Edges on Airplane Wings (1933)

NASA Technical Reports Server (NTRS) · leaf 18

An illustration from The Effect on Lift, Drag, and Spinning Characteristics of Sharp Leading Edges on Airplane Wings, 1933, leaf 18
Angle of attack,(degrees) Figure 2.- Aerodynamic charac teri3tics of the Clark Y, Clark Y-A and Clark Y-B airfoils. c5q*

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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