Effect of interstage bleed on rotating stall and blade vibration in a 13-stage axial-flow compressor in a turbojet engine

Author: Calvert, Howard F.
Additional Authors: Johnson, D. F.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56I06
Link: https://digital.library.unt.edu/ark:/67531/metadc62934/

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