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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