Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively
| Author: | Patterson, Elizabeth W. |
|---|---|
| Year: | 1958 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-4322 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57141/ |