NASA NTRS · 19740000067
Computer program for predicting off-design performance of centrifugal compressors
Abstract
Complete 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.
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Galvas, M. R.. 1974-08-01. Computer program for predicting off-design performance of centrifugal compressors. https://ntrs.nasa.gov/citations/19740000067
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