Wind-tunnel investigation of ailerons on a low-drag airfoil. : 3 - The effect of tabs /

Wind-tunnel investigation of ailerons on a low-drag airfoil. : 3 - The effect of tabs / by Ralph W. Holtzclaw and Robert M. Crane.

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An investigation was made of the effects of 0.20 aileron-chord tabs on an NACA 66,2-216 airfoil equipped with a 0.20-airfoil-chord plain sealed aileron. The aileron profiles considered consisted of one profile conforming to the normal NACA NACA 66,2-216 ordinates and a profile consisting of straight...

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Bibliographic Details
Main Author: Holtzclaw, Ralph W.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Ames Research Center
Other Authors: Crane, Robert M.
Other title:NACA Wartime Reports. Series A.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1944]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. A18.
Subjects:
Airplanes > Fighter planes.
Aerofoils.
Ailerons.
Tabs (Airplanes)
Hinge moments (Aerodynamics)
Wind tunnel testing.

Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/A18
Y 3.N 21/5:11/A18 Available Place a Hold

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