Flight Investigation of Lateral Control Devices for Use with Full-Span Flaps (1936)
NASA Technical Reports Server (NTRS) · leaf 9
o .4* ^ .070 C <- !§/ .080 ^§ £.050 65 75 85 95 105 115 125 135 to Air speed, feet per second Figure 7.—Variation of maximum angular velocity and acceleration with 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… … Lift coefficient, CL Figure 11— Comparative curves of rolling-moment criterion for standard, retract- able, and narrow-chord ailerons. one of the two elements constituting the rolling action, 70 80 90 100 110 120 130 Air speed, feet per second should be as large as possible. It is limited only by…
NASA Technical Reports Server (NTRS)
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