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Some Effects of Blade Trailing-Edge Thickness on Performance of a Single-Stage Axial-Flow Compressor
Author:
Moses, J. J.
Year:
1951
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E51F28
Link:
https://digital.library.unt.edu/ark:/67531/metadc58924/
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