Aerodynamic characteristics of several modifications of a 0.45-scale model of the vertical tail of the Curtiss XP-62 airplane / by John G. Lowry, Thomas R. Turner, and Robert B. Liddell.

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Bibliographic Details
Main Author: Lowry, John G.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Turner, Thomas R., Liddell, Robert B.
Other title:NACA Wartime Reports. Series L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, [1946]
Series:Wartime Reports (United States. National Advisory Committee for Aeronautics) ; no. L736.
Subjects:
Description
Abstract:The 0.45-scale model of the Curtiss XP-62 vertical tail surface mounted on a stub fuselage was tested in the Langley 7- by 10-foot tunnel. The aerodynamic characteristics of the vertical tail with a plain rudder, two amounts of overhang and an internal balance are presented. Tab characteristics on the plain rudder are also presented.
Item Description:NACA Wartime Report L-736.
Originally issued as NACA as Advance Confidential Report L6F27 (July 1946)
Prepared at the Langley Memorial Aeronautical Laboratory, Langley Field, Virginia.
Physical Description:9 pages, 34 unnumbered pages : illustrations ; 27 cm.
Bibliography:Includes bibliographical references.