Low-Speed Investigation of Aileron and Spoiler Characteristics of a Wing Having 42 Degrees Sweepback of the Leading Edge and Circular-Arc Airfoil Sections at Reynolds Numbers of Approximately 6.0 X 10(Exp 6)
| Author: | Spooner, Stanley H. |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9A07 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58210/ |