Pressure distribution at Mach numbers up to 0.90 on a cambered and twisted wing having 40 degrees of sweepback and an aspect ratio of 10, including the effects of fences
| Author: | Boltz, Frederick W |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A52K20 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59132/ |