Wind-tunnel investigation of the boundary layer and wake and their relation to airfoil characteristics - NACA 65₁-012 airfoil with a true contour flap and a beveled-trailing-edge flap / Robert A. Mendelsohn.

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Bibliographic Details
Main Author:	Mendelsohn, Robert A.
Corporate Author:	United States. National Advisory Committee for Aeronautics
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series:	Technical note (United States. National Advisory Committee for Aeronautics) ; 1304.
Subjects:	Aerofoils > Testing. Boundary layer. Wakes (Aerodynamics) Flaps (Airplanes) Trailing edges (Aerodynamics) Wind tunnel testing.

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Holdings details from PASCAL Offsite
Call Number:	Y 3.N 21/5:6/1304
Y 3.N 21/5:6/1304	Available Place a Hold