Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane / Leonard Sternfield.

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Bibliographic Details
Main Author: Sternfield, Leonard
Corporate Author: United States. National Advisory Committee for Aeronautics
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1950.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 2233.
Subjects:

MARC

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245 1 0 |a Some effects of nonlinear variation in the directional-stability and damping-in-yawing derivatives on the lateral stability of an airplane /  |c Leonard Sternfield. 
260 |a Washington, D.C. :  |b National Advisory Committee for Aeronautics,  |c 1950. 
300 |a 19 pages :  |b illustrations ;  |c 28 cm. 
336 |a text  |b txt  |2 rdacontent. 
337 |a unmediated  |b n  |2 rdamedia. 
338 |a volume  |b nc  |2 rdacarrier. 
490 1 |a National Advisory Committee for Aeronautics. Technical Note ;  |v no. 2233. 
500 |a "November 1950." 
500 |a NACA TN Number 2233. 
504 |a Includes bibliographical references. 
520 3 |a The effect of nonlinear stability derivatives on the lateral stability of an airplane is analyzed. Motions are calculated on the assumption that the values of the directional-stability derivative and the damping-in-yawing derivative are functions of the angle of sideslip. The application of the Laplace transform to the calculation of an airplane motion when certain types of nonlinear derivatives are present is described in detail. 
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650 0 |a Stability of airplanes, Lateral.  |0 http://id.loc.gov/authorities/subjects/sh85127187. 
650 0 |a Yawing (Aerodynamics)  |0 http://id.loc.gov/authorities/subjects/sh85149046. 
650 7 |a Stability of airplanes, Lateral.  |2 fast  |0 (OCoLC)fst01131215. 
650 7 |a Yawing (Aerodynamics)  |2 fast  |0 (OCoLC)fst01182552. 
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