Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section
| Author: | Smith, Hamilton A. |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2074 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55451/ |