Inside Out Library · Explore

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

NASA Technical Reports Server (NTRS) · leaf 19

An illustration from The Effect on Lift, Drag, and Spinning Characteristics of Sharp Leading Edges on Airplane Wings, 1933, leaf 19
o … Angle of attack, (degrees) Figure 3. -Variation of normal force coefficient with angle of attack.

NASA Technical Reports Server (NTRS)

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

More pictures from The Effect on Lift, Drag, and Spinning Characteristics of Sharp Leading Edges on Airplane Wings

More like this