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Free-flight performance of 16-inch-diameter supersonic ram-jet units 1: four units designed for combustion-chamber-inlet Mach number of 0.12 at free-stream Mach number of 1.6 (units A-2, A-3, A-4, and A-5)
| Author: | Carlton, William W. |
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| Year: | 1949 |
| Document Type: | N/A |
| Series: | NACA Research Memorandums |
| Report Number: | NACA-RM-E9F22 |
| Link: | https://digital.library.unt.edu/ark:/67531/metadc58252/ |
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