The effects of Mach number and Reynolds number on the aerodynamic characteristics of several 12-percent-thick wings having 35 degrees of sweepback and various amounts of camber
| Author: | Tinling, Bruce E. |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A50K27 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58776/ |