Aerodynamic characteristics of a 6-percent-thick symmetrical double-wedge airfoil at transonic speeds from tests by the NACA wing-flow method
| Author: | Lina, Lindsay J. |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9A12 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58214/ |