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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