A forced-oscillation method for dynamic- stability testing

• 1 September 1964
• journal article
• Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
• Vol. 1  (5) , 304-305
• https://doi.org/10.2514/3.43598

Abstract

Keywords

• OSCILLATIONS
• YAW
• FREE FLIGHT
• STABILITY
• DAMPING