Longitudinal-control effectiveness and downwash characteristics at a Mach number of 1.24 of a 1/30-scale semispan model of the Bell X-5 airplane as determined by the NACA wing-flow method
| Author: | Sawyer, Richard H. |
|---|---|
| Additional Authors: | Kennedy, Robert M. |
| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L50K15 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58759/ |