A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9
| Author: | Mitcham, Grady L. |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56K19 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63228/ |