Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8 x 10(exp 6) to 11.0 x 10(exp 6)
| Author: | Schaefer, Raymond F. |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-1998 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55386/ |