naca-rm-e58f20a
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- October 18, 2017 Create Date
- October 18, 2017 Last Updated
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National Advisory Committee for Aeronautics, Research Memorandum - Design and Experimental Investigation of a Single Stage Turbine with a Rotor Entering Relative Mach Number of 2
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naca-rm-e58f20a Design and Experimental Investigation of a Single Stage Turbine with a Rotor Entering Relative Mach Number of 2.pdf | Download |
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