Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6
| Author: | Unangst, John R. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L55I13a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc61634/ |