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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
| Content Provider | University of North Texas |
|---|---|
| Author | O'Kelly, Burke R. Lundstrom, Reginald R. Lauten, William T. Jr. |
| Organization | Langley Aeronautical Laboratory |
| Description | Free flight tests of 45-deg swept wings of 3.15 aspect ratio and 0.54 taper ratio to measure wing damping and possible transonic flutter. |
| File Format | |
| Archival Resource Key | ark:/67531/metadc52896 |
| Language | English |
| Publisher Date | 2019-01-10 |
| Access Restriction | Open |
| Subject Keyword | auxiliary systems aircraft wings |
| Content Type | Text |
| Resource Type | Report |