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Low-speed Characteristics in Pitch of a 42 Degree Sweptback Wing with Aspect Ratio 3.9 and Circular-arc Airfoil Sections

Robert H. Nealy, William Koven

Abstract

Report presenting tests in a pressure tunnel to determine the low-speed pitch characteristics of a 42 degree sweptback wing with circular-arc airfoil sections. Information regarding the characteristics of basic wing, leading-edge flap investigation, and effects of fuselage are provided.

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Available abstract

Key concepts: Airfoil, Wing, Fuselage, Arc (geometry), Leading edge, Degree (music), Structural engineering, Wing configuration