The Effects of Static Margin and Rotational Damping in Pitch on the Longitudinal Stability Characteristics of an Airplane as Determined by Tests of a Model in the NACA Free-Flight Tunnel
| Author: | Campbell, John P. |
|---|---|
| Year: | 1944 |
| Document Type: | N/A |
| Series: | NACA Wartime Reports |
| Report Number: | NACA-WR-L-55, NACA-ARR-L4F02 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60989/ |