Title: Wind-Tunnel Investigation of the Effects of a Fence and a Leading-Edge Notch on the Aerodynamic Loading Characteristics in Pitch of a 45 Degree Sweptback Wing at High Subsonic Speeds
Abstract: Report presenting an investigation in the high speed tunnel to determine the aerodynamic loading characteristics of a 45 degree sweptback wing of aspect ratio 4, taper ratio 0.6, and an NACA 65A006 airfoil section. The effects of fences and leading-edge notches over a range of Mach numbers and angles of attack were also explored. Results regarding chordwise load distributions and lateral center of pressure are provided.
Publication Year: 1953
Publication Date: 1953-10-20
Language: en
Type: article
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