Investigation of Flap-type Ailerons on an Untapered Wing Having an Aspect Ratio of 3.7, 45 Degree Sweepback, and an NACA 65A009 Airfoil Section PDF Download

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Investigation of Flap-type Ailerons on an Untapered Wing Having an Aspect Ratio of 3.7, 45 Degree Sweepback, and an NACA 65A009 Airfoil Section

Investigation of Flap-type Ailerons on an Untapered Wing Having an Aspect Ratio of 3.7, 45 Degree Sweepback, and an NACA 65A009 Airfoil Section PDF Author: Richard G. MacLeod
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 18

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Book Description
An investigation to determine the lateral control characteristics of a 20-percent-chord flap-type aileron of various spans on a semispan wing-fuselage model was made in the transonic speed range. The wing of the model had 45 degrees of sweepback, an aspect ratio of 3.7, a taper ratio of 1.0, and an NACA 65A009 airfoil section parallel to the free stream. Rolling moments were obtained through a small range of angles of attack and aileron deflections. Lift data on the complete model are also included.