Theoretical and analog studies of the effects of nonlinear stability derivatives on the longitudinal motions of an aircraft in response to step control deflections and to the influence of proportional automatic control

Author: Curfman, Howard J., Jr.
Year: 1950
Document Type: N/A
Series: NACA Technical Reports
Report Number: NACA-TR-1241
Link: https://digital.library.unt.edu/ark:/67531/metadc65579/

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