Calculation of the aerodynamic characteristics of tapered wings with partial-span flaps (1939)
NASA Technical Reports Server (NTRS) · leaf 16
13 TAPERED WINGS WITH PARTIAL-SPAN FLAPS … 4 5 6 1,000,000 2 3 4 5 6 10,000,000 6 1,000,000 4 5 6 10,000,000 Reynolds Number Figure 22.—Scale-effect corrections for Cimoi. In order to obtain the section maximum lift coefficient at the desired Reynolds Number, apply to the standard-test value the increment indicated by the curve that…
NASA Technical Reports Server (NTRS)
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