Experimental studies of flutter of buckled rectangular panels at Mach numbers from 1.2 to 3.0 including effects of pressure differential and of panel width-length ratio
| Author: | Sylvester, Maurice A. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55I30 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61777/ |