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Internal performance at Mach number to 2.0 of two auxiliary inlets immersed in fuselage boundary layer
| Author: | Pennington, Donald B |
|---|---|
| Year: | 1954 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E53L28b |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc64496/ |
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