Experimental study of the effects of finite surface disturbances and angle of attack on the laminar boundary layer of an NACA 64A010 airfoil with area suction
| Author: | Schwartzberg, Milton A. |
|---|---|
| Year: | 1952 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2796 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56369/ |