 |
|
Full-scale wind-tunnel tests of a 35 degree swept-wing fighter airplane with a spoiler-slot-deflector lateral control system
| Author: | Scallion, William I. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56D18 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62529/ |
Search developed and maintained by the University of Washington Libraries
Copyright 2010