Analysis of coolant flow and pressure requirements for a return-flow turbine rotor blade design using hydrogen, helium, or air as coolant

Author: Slone, Henry O.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E57B18
Link: https://digital.library.unt.edu/ark:/67531/metadc63211/

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