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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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