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Rotary balance data for a single engine general aviation design having a high aspect-ratio canard for an angle-of-attack range of 30 deg to 90 deg

W. J. Mulcay, Rebecca Rose

Abstract

Aerodynamic characteristics obtained in a helical flow environment utilizing a rotary balance located in the Langley spin tunnel are presented in plotted form. The configurations tested included the basic airplane, various control deflections, two canard locations, and wing leading edge modifications, as well as airplane components.

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Available abstract

Key concepts: Airplane, Aerodynamics, Aerospace engineering, Range (aeronautics), Wing, Aviation, Angle of attack, Flight control surfaces