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Experimental Investigation of the Effect of Circumferential Inlet Flow Distortion on the Performance of a Five-Stage Axial-Flow Research Compressor with Transonic Rotors in All Stages
Author:
Robbins, William H.
Year:
1958
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E57J17
Link:
https://digital.library.unt.edu/ark:/67531/metadc64157/
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