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Investigation of two-stage air-cooled turbine suitable for flight at Mach number of 2.5 2: blade design
Author:
Miser, James W.
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E56K06
Link:
https://digital.library.unt.edu/ark:/67531/metadc62782/
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