A Simple method of estimating the subsonic lift and damping in roll of sweptback wings / Edward C. Polhamus.

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Bibliographic Details
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Main Author: Polhamus, Edward C. (Edward Charles), 1923-2001
Corporate Author: United States. National Advisory Committee for Aeronautics
Other title:Technical report archive and image library.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1949.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1862.
Subjects:
Description
Abstract:A method of modifying existing correction factors of lifting-surface theory to account approximately for the effects of sweep has been derived, and these factors have been applied to existing lifting-line theories for the lift and damping in roll of swept wings. A comparison with experimental data in the low-speed and low lift range indicated good agreement for wings of any plan form. If the Glauert-Prandtl transformation is used, the formulas obtained can be applied to swept wings at subsonic speeds below the critical speed.
Item Description:"April 1949."
NACA TN Number 1862.
Physical Description:20 pages : illustrations ; 28 cm.
Bibliography:Includes bibliographical references.
Action Note:will digitize