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Investigation of a High-Flow Transonic-Compressor Inlet Stage Having a Hub-Tip Radius of 0.35
Author:
Felix, A. Richard
Year:
1958
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L58A08
Link:
https://digital.library.unt.edu/ark:/67531/metadc63716/
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