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: | NASA-TM-79830, NACA-TN-2796 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc53335/ |