Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing
| Author: | Schneider, William C. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L56B14 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc62251/ |