skip to content
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/
< New search