A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2
| Author: | Phelps, E. Ray |
|---|---|
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A57A10 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53055/ |