Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model / Leslie E. Schneiter and Rodger L. Naeseth.

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Bibliographic Details
Main Author: Schneiter, Leslie E.
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Naeseth, Rodger L.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1948.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 1738.
Subjects:

MARC

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245 1 0 |a Wind-tunnel investigation at low speed of the lateral control characteristics of ailerons having three spans and three trailing-edge angles on a semispan wing model /  |c Leslie E. Schneiter and Rodger L. Naeseth. 
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300 |a 52 pages :  |b illustrations ;  |c 27 cm. 
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490 1 |a National Advisory Committee for Aeronautics. Technical Note ;  |v no. 1738. 
500 |a "November 1948." 
500 |a NACA TN Number 1738. 
504 |a Includes bibliographical references. 
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650 0 |a Ailerons.  |0 http://id.loc.gov/authorities/subjects/sh85002551. 
650 0 |a Flaps (Airplanes)  |0 http://id.loc.gov/authorities/subjects/sh85049001. 
650 0 |a Stability of airplanes, Lateral.  |0 http://id.loc.gov/authorities/subjects/sh85127187. 
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