Wind-tunnel investigation of control-surface characteristics. : 20 - Plain and balanced flaps on an NACA 0009 rectangular semispan tail surface / by I. Elizabeth Garner.

Correlation is established between aerodynamic characteristics of control surfaces in two-dimensional and three-dimensional flow. Slope of lift curve was affected little by overhang and balance-nose shape, but increased by sealing flap-nose gap. Effectiveness of balancing tab was same for sealed pla...

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Bibliographic Details
Main Author: Garner, I. Elizabeth
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other title:NACA Wartime Reports. Series L.
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. L186.
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Norlin Library - Basement - Government Information - US

Holdings details from Norlin Library - Basement - Government Information - US
Call Number: Y 3.N 21/5:11/L186
Y 3.N 21/5:11/L186 Available Place a Hold