Effects of Wing Sweep, Horizontal-Tail Configuration, and a Ventral Fin on Static Stability Characteristics of a Model With a Wing of Aspect Ratio 3 at Mach Numbers From 2.29 to 4.65
| Author: | Jaquet, Byron M. |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58E06 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64404/ |