naca-rm-e9k25

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naca-rm-e9k25 Study of Flow Conditions and Deflection Angle at Exit of Two Dimensional Cascade of Turbine Rotor Blades at Critical and Supercritical Pressure Ratios.pdfDownload 

National Advisory Committee for Aeronautics, Research Memorandum - Study of Flow Conditions and Deflection Angle at Exit of Two Dimensional Cascade of Turbine Rotor Blades at Critical and Supercritical Pressure Ratios


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