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Effect of leading-edge geometry on boundary-layer transition at Mach 3.1
| Author: | Brinich, Paul F. |
|---|---|
| Year: | 1956 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3659 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc56630/ |
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