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The Calculated Effect of Various Hydrodynamic and Aerodynamic Factors on the Take-Off of a Large Flying Boat (1939)
NASA Technical Reports Server (NTRS) · leaf 17
3.0 _4 0 4 8 13 16 Angle of attack, deg. Fieura 1.- Lift and drag coefficients of a tapered airfoil witn various flap deflections. Ae=30, ground effect included.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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