A Theoretical Investigation of the Effect on the Lateral Oscillations of an Airplane of an Automatic Control Sensitive to Yawing Accelerations

Author: Beckhardt, Arnold R.
Year: 1950
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2006
Link: https://digital.library.unt.edu/ark:/67531/metadc55308/

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