Wind-tunnel investigation at low speed of a 45 degree sweptback untapered semispan wing of apsect ratio 1.59 equipped with various 25-percent-chord plain flaps / Harold S. Johnson and John R. Hagerman.

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Bibliographic Details
Main Author:	Johnson, Harold S.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Hagerman, John R.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2169.
Subjects:	Airplanes > Wings, Swept-back. Flaps (Airplanes) Lift (Aerodynamics) Drag (Aerodynamics) Pitching (Aerodynamics) Stability of airplanes, Lateral.

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Call Number:	Y 3.N 21/5:6/2169
Y 3.N 21/5:6/2169	Available Place a Hold