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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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