Title: Investigation of a 10-stage Subsonic Axial-flow Research Compressor II : Preliminary Analysis of Overall Performance
Abstract: Report presenting an investigation of the overall performance of a 20-inch-tip-diameter 10-stage compressor as the initial step to examine the problems encountered in an axial-flow compressor with a high pressure ratio per stage. The investigation was carried out over a range of weight flows and percentages of the design speed. Results regarding the part-speed efficiency, surge characteristics, overspeed characteristics, compressor discharge Mach number, and stage characteristics are provided.
Publication Year: 1952
Publication Date: 1952-05-16
Language: en
Type: article
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Cited By Count: 5
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