Theoretical investigation of the longitudinal response characteristics of a swept-wing fighter airplane having a pitch-attitude control system
| Author: | Stokes, Fred H. |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2882 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56890/ |