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Force and pressure characteristics for a series of nose inlets at Mach numbers from 1.59 to 1.99 1: conical spike all-external compression inlet with subsonic cowl lip
| Author: | Esenwein, Fred T. |
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| Year: | 1951 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E50J26 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58624/ |
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