The Effect at High Subsonic Speeds of a Flap-type Aileron on the Chordwise Pressure Distribution Near Midsemispan of a Tapered 35 Degree Sweptback Wing of Aspect Ratio 4 Having NACA 65A006 PDF Download

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The Effect at High Subsonic Speeds of a Flap-type Aileron on the Chordwise Pressure Distribution Near Midsemispan of a Tapered 35 Degree Sweptback Wing of Aspect Ratio 4 Having NACA 65A006

The Effect at High Subsonic Speeds of a Flap-type Aileron on the Chordwise Pressure Distribution Near Midsemispan of a Tapered 35 Degree Sweptback Wing of Aspect Ratio 4 Having NACA 65A006 PDF Author: Homer B. Wilson
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 89

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Book Description
This paper presents effects of the deflection of a flat-type aileron on the chordwise pressure distribution at the 46-percent-semispan station of a tapered 35 degree sweptback wing of aspect ratio 4 with an NACA 65A006 airfoil section. The tests were made at angles of attack from 0 to 20 degrees and at Mach numbers from 0.60 to 0.95 for aileron deflections from -30 to 30 degrees.