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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| Main Author: | |
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| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1950.
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2233. |
| Subjects: |
| Abstract: | 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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| Item Description: | "November 1950." NACA TN Number 2233. |
| Physical Description: | 19 pages : illustrations ; 28 cm. |
| Bibliography: | Includes bibliographical references. |
| Action Note: | committed to retain |