Results of initial wind-tunnel flutter experiments at low speed with a towed airplane model having a 40 degree sweptback wing of aspect ratio 3.62 equipped with pylon-mounted stores
| Author: | Martina, Albert P. |
|---|---|
| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54K17 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc60993/ |