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Laminar boundary layer on a circular cone in supersonic flow at a small angle of attack
| Author: | Moore, Franklin K |
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| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-2521 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc55913/ |
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