Wind-Tunnel Investigation of an NACA 0009 Airfoil With 0.25-and 0.50-Airfoil-Chord Plain Flaps Tested Independently and in Combination
| Author: | Spearman, M. Leroy |
|---|---|
| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-1517 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc54492/ |