Flight Investigation of Lateral Control Devices for Use with Full-Span Flaps (1936)
NASA Technical Reports Server (NTRS) · leaf 9
air 040 Q). speed for standard ailerons. O o 1.0 ^.020 C o _Retroctoble ailerons. -Flaps down I up Narrow-chord ailerons to -Flaps down- .010 to up •6b * 'Standard ailerons- £8 i i i °4 3 to .6 .8 1.0 1.2 1.4 1.6 1.9 2.0 Lift coefficient, CL M Figure 10.—Variation of Ci with Cl for standard,… … Air speed, feet per second should be as large as possible. It is limited only by Figure 9.—Variation of maximum angular velocity and acceleration with air speed structural considerations and the possible discomfort for narrow-chord ailerons. that the acceleration produced by it may cause the…
NASA Technical Reports Server (NTRS)
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