Effects of rate of flap deflection on flap hinge moment and wing lift through the Mach number range from 0.32 to 0.87
| Author: | Turner, Thomas R. |
|---|---|
| Year: | 1953 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L53E11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc59685/ |