Wind-Tunnel and Flight Tests of Slot-lip Ailerons (1937)
NASA Technical Reports Server (NTRS) · leaf 12
of this upward (>()° in all cases and were located at 0.10, 0.30, moment with aileron deflection was not uniform. and 0.55cw. With the slots open the rolling moments are appreciably higher below the stall but are definitely With the (lap deflected, the difference between the two |8 X%'~-90 -80 -70… … Angle of attach, af ,deg. Angle of attack, d ,deg. Figure 18.—Effect of slot-lip aileron location on rolling- and yawing-moment coefficients, 8a up 40°, down 12°. lower above the stall. The yawing-moment coeffi- slot shapes was even greater, as may be seen by com- cients are lowrer with the slots…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
