An investigation of the control effectiveness of tip ailerons and spoilers on a low-aspect-ratio trapezoidal-wing airplane model at Mach numbers from 1.55 to 2.35

Wong, Norman D.
naca-rm-a57i26a
1957


Results are presented, in graphical and tabular form, from a wind-tunnel investigation of the static longitudinal and lateral characteristics of a complete wing, fuselage, and tail combination at Mach numbers from 1.55 to 2.35 and at a Reynolds number of approximately 1.4 x 10 to the 6th.

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