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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 C. [wind tunnel tests

W. J. Mulcay, Rebecca Rose

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Key concepts: Range (aeronautics), General aviation, Wind tunnel, Angle of attack, Balance (ability), Wing, Aviation, 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 C. [wind tunnel tests — Research Paper | ScholarLens