Experimental Flutter Results for Cantilever-Wing Models at Mach Numbers Up to 3.0
| Author: | Tuovila, W. J. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55E11 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61470/ |