Effects of leading-edge slats on the aerodynamic characteristics of a 45 degree sweepback wing-fuselage configuration at Mach numbers of 0.4 to 1.03
| Author: | Runckel, Jack F. |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53F23 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59785/ |