An investigation of a lifting 10-percent-thick symmetrical double-wedge airfoil at mach number up to 1
| Author: | Humphreys, Milton D |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3306 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57312/ |