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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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