An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.59
| Author: | Cooper, Morton |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50C24 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58574/ |