NASA NTRS · 19850000531
Predicting the Performance of an Axial-Flow Compressor
Abstract
Stage-stacking computer code (STGSTK) developed for predicting off-design performance of multi-stage axial-flow compressors. Code uses meanline stagestacking method. Stage and cumulative compressor performance calculated from representative meanline velocity diagrams located at rotor inlet and outlet meanline radii. Numerous options available within code. Code developed so user modify correlations to suit their needs.
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Steinke, R. J.. 1986-03-01. Predicting the Performance of an Axial-Flow Compressor. https://ntrs.nasa.gov/citations/19850000531
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