Two-dimensional cascade investigation of the maximum exit tangential velocity component and other flow conditions at the exit of several turbine blade designs at supercritical pressure ratios

Author: Hauser, Cavour H
Year: 1951
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E51F12
Link: https://digital.library.unt.edu/ark:/67531/metadc59060/

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