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Experimental noise studies of inlet-guide- vane-rotor-stator interactions for a single- stage axial-flow compressorNoise generation in axial flow compressors - acoustic data in form of noise radiation patterns from inlet-guide-vane-rotor-stator interactions
Document ID
19660001362
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Copeland, W. L. (NASA Langley Research Center Hampton, VA, United States)
Crigler, J. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1965
Subject Category
Physics, General
Report/Patent Number
NASA-TM-X-56903
Report Number: NASA-TM-X-56903
Accession Number
66N10651
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ROTOR BLADE
AXIAL FLOW COMPRESSOR
WAVE INTERACTION
STATOR BLADE
ACOUSTICS
NOISE MEASUREMENT

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