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Analysis of fully stalled compressorAn analysis yields a model for energy transfer in compressor stages operating in the closed-throttle condition. The derivation indicates that three geometry parameters (hub/tip ratio, aspect ratio, and rotor blade setting angle) influence the values of pressure coefficient when the compressor flow is close to zero.
Document ID
19860053742
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rostafinski, W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
May 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 86-1123
Report Number: AIAA PAPER 86-1123
Accession Number
86A38480
Distribution Limits
Public
Copyright
Other

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