Aerodynamic characteristics at Mach number of 4.06 of a typical supersonic airplane model using body and vertical-tail wedges to improve directional stability
| Author: | Dunning, Robert W |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L57I10 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc63668/ |