Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model /

Wind-tunnel tests of a piston-type control booster on an airfoil and aileron model / by J.D. Bird and Robert A. Mendelsohn.

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Measurements of control moments were made in the NACA stability tunnel to determine the operational characteristics of a piston-type control booster on an aileron. The tests were made on a 6-foot-span and 4-foot-chord airfoil which extended completely across the 6-foot-square test section.

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Bibliographic Details
Main Author: Bird, J. D.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Mendelsohn, Robert A.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1943]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L494.
Subjects:
Ailerons.
Aerofoils.
Airplanes > Control systems.
Pistons.
Hinge moments (Aerodynamics)
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/L494
Y 3.N 21/5:11/L494 Available Place a Hold

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