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NACA procedure for flight tests of aileron characteristics of airplanes

Harold I Johnson

Abstract

Report describes the standard procedure that NACA used for evaluating the aileron characteristics of airplanes. The variables measured in the testing are rolling velocity, aileron positions, aileron stick forces or tangential wheel force, indicated airspeed, altitude, free-air temperature, and rudder position. The step-by-step flight procedure is described and information regarding evaluation of the control data and general suggestions is included.

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Available abstract

Key concepts: Aileron, Airspeed, Rudder, Aeronautics, Engineering, Wing, Marine engineering, Aerospace engineering