A Lifting-surface-theory solution and tests of an elliptic tail surface of aspect ratio 3 with a 0.5-chord 0.85-span elevator /

A Lifting-surface-theory solution and tests of an elliptic tail surface of aspect ratio 3 with a 0.5-chord 0.85-span elevator / Robert S. Swanson, Stewart M. Crandall, and Sadie Miller.

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Bibliographic Details
Main Author: Swanson, Robert S.
Corporate Authors: United States. National Advisory Committee for Aeronautics, Langley Aeronautical Laboratory
Other Authors: Crandall, Stewart M., Miller, Sadie
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1947.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1275.
Subjects:
Airplanes > Tail surfaces.
Elevators (Airplanes)
Aspect ratio (Aerofoils)
Lift (Aerodynamics)
Wind tunnel testing.
Description
Item Description:"May 1947."
NACA TN Number 1275.
Physical Description:32 pages, 22 unnumbered pages : illustrations ; 27 cm.
Bibliography:Includes bibliographical references.

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