Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-Wing Fighter-Bomber-Type Airplane With a Top Inlet at Mach Numbers From 1.6 to 2.35
| Author: | Gnos, A. Vernon |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A57K20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64226/ |