Free-flight Tests of 45 Deg Swept Wings of Aspect Ratio 3.15 and Taper Ratio 0.54 to Measure Wing Damping of the First Bending Mode and to Investigate the Possibility of Flutter at Transonic Speeds
| Author: | O'Kelly, Burke R. |
|---|---|
| Additional Authors: | Lundstrom, Reginald R. |
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L54C22 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc52896/ |