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Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 deg to 90 deg. 1: Low-wing model A. [fluid flow and vortices data for general aviation aircraft to determine aerodynamic characteristics for various designs

R. S. Hultberg, W. J. Mulcay

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Key concepts: Angle of attack, Vortex, Range (aeronautics), Flow (mathematics), Mechanics, General aviation, Balance (ability), Aerospace engineering

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Rotary balance data for a typical single-engine general aviation design for an angle-of-attack range of 8 deg to 90 deg. 1: Low-wing model A. [fluid flow and vortices data for general aviation aircraft to determine aerodynamic characteristics for various designs — Research Paper | ScholarLens