Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45° swept-back wing of aspect ratio 8 at Reynolds numbers from 1.5 x 10⁶ to 4.8 x 10 as determined by pressure distributions, force tests, and calculations, by George L. Pratt et al.

Title:	Effects of twist and camber on the low-speed longitudinal stability characteristics of a 45° swept-back wing of aspect ratio 8 at Reynolds numbers from 1.5 x 10⁶ to 4.8 x 10 as determined by pressure distributions, force tests, and calculations
Author:	Pratt, George L.
Author:	United States. National Adviosry Committee for Aeronautics
Author:	Langley Aeronautical Laboratory
Note:	National Advisory Committee for Aeronautics, 1952

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Subject:	Airplanes -- Wings, Swept-back
Subject:	Boundary layer control
Subject:	Camber (Aerofoils)
Subject:	Flaps (Airplanes)
Subject:	Reynolds number
Subject:	Stability of airplanes, Longitudinal
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