Wind-Tunnel Flutter Tests at Mach Numbers Up to 3.0 of Boeing Wing Models for Weapons System 110A: Coord. No. AF-AM-108
| Author: | Levey, G. M. |
|---|---|
| Additional Authors: | Tuovila, W. J. |
| Year: | 1957 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-SL57J11a |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64963/ |