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:

MARC

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245 1 2 |a 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 /  |c Robert S. Swanson, Stewart M. Crandall, and Sadie Miller. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1947. 
300 |a 32 pages, 22 unnumbered pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a National Advisory Committee for Aeronautics. Technical Note ;  |v no. 1275. 
500 |a "May 1947." 
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504 |a Includes bibliographical references. 
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650 0 |a Aspect ratio (Aerofoils)  |0 http://id.loc.gov/authorities/subjects/sh85008696. 
650 0 |a Lift (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85076855. 
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