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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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