Investigation of turbines suitable for use in a turbojet engine with high compressor pressure ratio and low compressor tip-speed II : velocity-diagram study of turbine for engine operation with constant exhaust-nozzle area

Author: Davison, Elmer H
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E52D14
Link: https://digital.library.unt.edu/ark:/67531/metadc59254/

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