Longitudinal stability and control characteristics at Mach numbers of 1.41 and 2.01 of a 67 degree swept-wing airplane configuration with canard control surfaces
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L58E20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64251/ |