Experimental study of the effects of finite surface disturbances and angle of attack on the laminar boundary layer of an NACA 64A010 airfoil with area suction / Milton A. Schwartzberg and Albert L. Braslow.

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Bibliographic Details
Main Author:	Schwartzberg, Milton A.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Other Authors:	Braslow, Albert L.
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1952.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 2796.
Subjects:	Airplanes > Wings. Aerofoils. Angle of attack (Aerodynamics) Laminar flow. Laminar boundary layer. Wind tunnel testing.

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Call Number:	Y 3.N 21/5:6/2796
Y 3.N 21/5:6/2796	Available Place a Hold