Experimental Investigation of a Transonic Aspirated Compressor

The experimental investigation of a transonic aspirated stage demonstrating the application of boundary layer aspiration to increase stage work is presented. The stage was designed to produce a pressure ratio of 1.6 at a tip speed of 750ft∕s resulting in a stage work coefficient of 0.88. The primary...

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Veröffentlicht in:	Journal of turbomachinery 2005-04, Vol.127 (2), p.340-348
Hauptverfasser:	Schuler, Brian J., Kerrebrock, Jack L., Merchant, Ali
Format:	Artikel
Sprache:	eng
Schlagworte:	Applied sciences Continuous cycle engines: steam and gas turbines, jet engines Engines and turbines Exact sciences and technology Mechanical engineering. Machine design
Online-Zugang:	Volltext
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