Wing-tunnel investigation at Mach numbers from 0.50 to 1.29 of an all-movable triangular wing of aspect ratio 4 alone and with a body
| Author: | Stivers, Louis S. |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-A9L01 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58401/ |