Wind-tunnel investigation of shielded horn balancees and tabs on a 0.7-scale model of XF6F vertical tail surface / by John G. Lowry, James A. Maloney, and I. Elizabeth Garner.

Results of subject tests indicate the difficulty of obtaining closely balanced rudder surfaces for most tail assemblies with shielded horns and maintaining a near zero rate-of-change of hinge-moment coefficient without an additional balancing device. A comparison is made between shielded and unshiel...

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Main Author: Lowry, John G.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Maloney, James A., Garner, I. Elizabeth
Other title:NACA Wartime Reports. Series L.
Technical report archive and image library.
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. L516.
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Norlin Library - Basement - Government Information - US

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Call Number: Y 3.N 21/5:11/L516
Y 3.N 21/5:11/L516 Available Place a Hold