Characteristics of a Single Float Seaplane During Take-off (1925)
NASA Technical Reports Server (NTRS) · leaf 11
hough somewhat in error due to ground inter- Meihod of control Fig. 22.- Time used for each stage by different take-o/T methods ference. The ahsohite Uft coefficient, C'l, is derived from tlie vek)city curve and is also plotted in Figure 23. The range of take-off speeds is here shown to he from 41… … Fig. 23.—Velocity and lift coeOiciont at various angles of take-olT formaUCC and should be kuOW^U.
NASA Technical Reports Server (NTRS)
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