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Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing
| Author: | Wolff, E B |
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| Year: | 1926 |
| Document Type: | N/A |
| Series: | NACA Technical Memorandums |
| Report Number: | NACA-TM-354 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc65163/ |
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