Investigation of effect of span and spanwise location of plain and stepped spoiler ailerons on lateral control characteristics of a wing with leading edge swept back 51.3 degrees
| Author: | Fischel, Jack |
|---|---|
| Year: | 1950 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9K02 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58340/ |