Effects on control effectiveness of systematically varying the size and location of trailing-edge flaps on a 45 degrees sweptback wing at a Mach number of 1.9
| Author: | Jacobsen, Carl R. |
|---|---|
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L51I26 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59059/ |