Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(1)-210 airfoil section /

Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(1)-210 airfoil section / by William J. Underwood, Albert L. Braslow, and Jones F. Cahill.

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An investigation was made of three interchangeable sealed-gap 0.20-airfoil-chord plain ailerons of different contour on the NACA 65(sub 1)-210 airfoil section. The three aileron contours tested were the true airfoil contour, straight sides, and a beveled trailing edge. The effects of aileron contour...

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Bibliographic Details
Main Author: Underwood, William J.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Braslow, Albert L., Cahill, Jones F.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1945]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L151.
Subjects:
Aerofoils.
Ailerons.
Hinge moments (Aerodynamics)
Surface roughness.
Wind tunnel testing.
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/L151
Y 3.N 21/5:11/L151 Available Place a Hold

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