A theoretical analysis of the effect of aileron inertia and hinge moment on the maximum rolling acceleration of airplanes in abrupt aileron rolls

Author: Bailey, F. J., Jr.
Year: 1942
Document Type: N/A
Series: NACA Wartime Reports
Report Number: NACA-WR-L-302, NACA-ARR
Link: https://digital.library.unt.edu/ark:/67531/metadc61020/

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