Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6)
| Author: | Lange, Roy H. |
|---|---|
| Year: | 1948 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L8D30 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57702/ |