Aerodynamic study of a wing-fuselage combination employing a wing swept back 63 degrees : characteristics at a Mach number of 1.53 including effect of small variations of sweep
| Author: | Madden, Robert T |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A8J04 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57831/ |