Wind-Tunnel and Flight Tests of Slot-lip Ailerons (1937)
NASA Technical Reports Server (NTRS) · leaf 11
8 REPORT NO. 602—NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Aileron deflection, 6a ,deg. Figure 14.—Rolling- and yawing-moment coefficients due to slot-lip ailerons at 0.10c„. 10 -70 SO SO -40 SO -20 -10 0 'To SO -70 SO SO -40 -30 -20 10 SO SO Aileron deflection, 6a ,deg. Figure 15.—Rolling- and yawing-moment coefficients due to slot-lip ailerons at…
NASA Technical Reports Server (NTRS)
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