Transonic free-flight investigation of the longitudinal aerodynamic characteristics of a 1/10-scale steel-wing of the Northrop MX-775A missile with leading-edge extensions, inboard trailing-edge flaps, and a speed brake on the vertical tail
| Author: | Arbic, Richard G |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL55B07 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61180/ |