An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc section and 40 degree sweepback: a pressure-distribution study of the aerodynamic characteristics of the wing at Mach number 1.40
| Author: | Smith, Norman F. |
|---|---|
| Additional Authors: | Kainer, Julian H. |
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51C06 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58815/ |