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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