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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 18
33,000 20,000 3,000 110 130 130 80 90 Speed, f.p.s. flaps set at 0°, Figure 3.- Effect of load coefficient, 0A , on take off, withNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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