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Charts of boundary-layer mass flow and momentum for inlet performance analysis mach number range, 0.2 to 5.0
| Author: | Simon, Paul C. |
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| Year: | 1955 |
| Document Type: | N/A |
| Series: | NACA Technical Notes |
| Report Number: | NACA-TN-3583 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc57906/ |
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