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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 ration, aspect ration, and rotor blade setting angle) influence the values of pressure coefficient when the compressor flow is close to zero.
Document ID
19860010886
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rostafinski, W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-87254
E-2944
NAS 1.15:87254
Report Number: NASA-TM-87254
Report Number: E-2944
Report Number: NAS 1.15:87254
Meeting Information
Meeting: Joint Fluid Mechanics, Plasma Dynamics and Laser Conference
Location: Atlanta, GA
Country: United States
Start Date: May 12, 1986
End Date: May 14, 1986
Sponsors: AIAA, American Society of Mechanical Engineers
Accession Number
86N20357
Funding Number(s)
PROJECT: RTOP 505-69-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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