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Investigation of the effect of velocity diagram on inlet total-pressure distortions through single-stage subsonic axial-flow compressors
Author:
Ashby, George C , Jr
Year:
1957
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L57A03
Link:
https://digital.library.unt.edu/ark:/67531/metadc63459/
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