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Hydrodynamic tests for determining the take-off characteristics of seaplanes (1923)
NASA Technical Reports Server (NTRS) · leaf 12
.030 .025 :0k J*>.020 -.03^.015^ -.02^.010^ 005- 0 30 £o 9c of incidence ' Aerodynamic Drag (lx).Model 1/20 size n Lift (ly).Tvith one float. Airspeed ^0 m/sec. * * * Aerodynamic Drag (Lx). Seaplane \7ith " Lift (Ly). one float. Airspeed lin/sec. Fig.2.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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