Low-speed longitudinal stability and lateral-control characteristics of a model of a 40 degree swept-wing fighter-type airplane at a Reynolds number of 9 x 10(exp 6)
| Author: | Bollech, Thomas V. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54B17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60199/ |