Low-speed, Large-scale Investigation of Aerodynamic Characteristics of a Semispan 49 Degree Sweptback Wing with a Fowler Flap in Combination with a Plain Flap, Slats, and Fences
Edward F Whittle, Stanley Lipson
Abstract
Edward F Whittle, Stanley Lipson
Abstract
Report presenting an investigation in the full-scale tunnel to determine the effects of a Fowler type slotted flap on the aerodynamic characteristics of a semispan 49.1 degree sweptback wing with NACA 65A006 airfoil sections streamwise, an aspect ratio of 3.78, and a taper ratio of 0.59. Results regarding the pitching-moment curve, effect of flap deflection, and lift increments are provided.
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Report presenting an investigation in the full-scale tunnel to determine the effects of a Fowler type slotted flap on the aerodynamic characteristics of a semispan 49.1 degree sweptback wing with NACA 65A006 airfoil sections streamwise, an aspect ratio of 3.78, and a taper ratio of 0.59. Results regarding the pitching-moment curve, effect of flap deflection, and lift increments are provided.
Key concepts: Airfoil, Wing, Aerodynamics, Deflection (physics), Lift (data mining), Pitching moment, Geology, Structural engineering