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Computer program for predicting off-design performance of centrifugal compressorsComplete knowledge of compressor overall geometry and working fluid total inlet conditions is required for program's use. On given speed line, compressor performance is calculated for range of inlet velocity levels. Working fluid state conditions and flow properties are calculated using mean stream line one-dimensional analysis.
Document ID
19740000067
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Galvas, M. R. (U. S. Army Air Mobility R and D Lab.)
Date Acquired
August 7, 2013
Publication Date
August 1, 1974
Subject Category
Mathematics And Information Sciences
Report/Patent Number
Report Number: LEW-12186
LEW-12186
Accession Number
74B10067
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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