Wind-tunnel investigation at subsonic and supersonic speeds of a fighter model employing a low-aspect-ratio unswept wing and a horizontal tail mounted well above the wing plane - longitudinal stability and control
| Author: | Smith, Willard G |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A54D05 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60776/ |