Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds
| Author: | Daley, Bernard N. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3424 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57708/ |