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Experimental Investigation of a Transonic Axial-Flow-Compressor Rotor Designed for Sonic Inlet Velocity with an Inlet Hub-Tip Radius of 0.35
Author:
Boxer, Emanuel
Year:
1956
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-L56F14
Link:
https://digital.library.unt.edu/ark:/67531/metadc62596/
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