High-Speed Wind-Tunnel Tests of an NACA 0009-64 Airfoil Having a 33.4-Percent-Chord Flap With an Overhang 20.1 Percent of the Flap Chord
| Author: | Stevenson, David B. |
|---|---|
| Year: | 1947 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-1417 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc54291/ |