Effects of Mach number variation between 0.07 and 0.34 and Reynolds number variation between 0.97 x 10(exp 6) and 8.10 x 10(exp 6) power on the maximum lift coefficient of a wing of NACA 64-210 airfoil sections
| Author: | Fitzpatrick, James E. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2753 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56398/ |