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FORTRAN program for predicting off-design performance of centrifugal compressorsA FORTRAN program for calculating the off-design performance of centrifugal compressors with channel diffusers is presented. Use of the program requires complete knowledge of the overall impeller and diffuser geometries. Individual losses are computed using analytical equations and empirical correlations which relate loss levels to velocity diagram characteristics and overall geometry. On a given speed line compressor performance is calculated for a range of inlet velocity levels. At flow rates between surge and choke, individual efficiency decrements, compressor overall efficiency, and compressor total pressure ratio are tabulated. An example case of performance comparison with a compressor built by a commercial engine manufacturer is presented to demonstrate the correlation with limited experimental data.
Document ID
19740001912
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Galvas, M. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
November 1, 1973
Subject Category
Aerodynamics
Report/Patent Number
E-7480
NASA-TN-D-7487
Report Number: E-7480
Report Number: NASA-TN-D-7487
Accession Number
74N10024
Funding Number(s)
PROJECT: RTOP 501-24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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