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Wind-Tunnel Flutter Tests at Mach Numbers up to 3.0 of Boeing Wing Models for Weapons System 110A
| 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/metadc53151/ |
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