An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line designed to produce a high critical Mach number
| Author: | Loftin, Laurence K., Jr. |
|---|---|
| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-1633 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc54726/ |