Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil /

Investigation of the variation of lift coefficient with Reynolds number at a moderate angle of attack on a low-drag airfoil / by Albert E. von Doenhoff and Neal Tetervin.

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An investigation of the boundary layer about the NACA 66,2-216, a = 0.6, airfoil section has been made in the NACA two-dimensional low-turbulence tunnel, in an attempt to find an explanation for the decreased slot of the lift curve observed for some of the low-drag sections outside the low-drag rang...

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Bibliographic Details
Main Author: Von Doenhoff, Albert E.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Tetervin, Neal
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1942]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L661.
Subjects:
Aerofoils.
Angle of attack (Aerodynamics)
Air flow.
Lift (Aerodynamics)
Drag (Aerodynamics)
Reynolds number.
Boundary layer.
Charts, diagrams, etc.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L661
Y 3.N 21/5:11/L661 Available Place a Hold

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