Effect of thickness, camber, and thickness distribution on airfoil characteristics at Mach numbers up to 1.0
| Author: | Daley, Bernard N |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3607 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57800/ |