Pressure Distributions and Force Tests of an NACA 65-210 Airfoil Section With a 50-Percent-Chord Flap
| Author: | Klein, Milton M. |
|---|---|
| Year: | 1947 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-1167 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55231/ |