The effectiveness at high subsonic Mach numbers of a 20-percent-chord plain trailing-edge flap on the NACA 65-210 airfoil section
| Author: | Stivers, Louis S , Jr |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3127 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57107/ |