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/ |