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Investigation of a 10-stage subsonic axial-flow research compressor V : effect of reducing inlet-guide-vane turning on over-all and inlet-stage performance
Author:
Budinger, Ray E
Year:
1954
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E53H10
Link:
https://digital.library.unt.edu/ark:/67531/metadc59693/
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