Wing-tunnel investigation at high subsonic speeds of the lateral-control characteristics of an aileron and a stepped spoiler on a wing with leading edge swept back 51.3 degrees
| Author: | Schneiter, Leslie E |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9D06 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58204/ |