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High-subsonic damping-in-roll characteristics of a wing with the quarter-chord line swept back 35 degrees and with aspect ratio 3 and taper ratio 0.6
| Author: | Myers, Boyd C , II |
|---|---|
| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-L9C23 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58262/ |
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