Wake, Shock, and Potential Field Interactions in a 1.5 Stage Turbine—Part I: Vane-Rotor and Rotor-Vane Interaction

The composition of the time-resolved surface pressure field around a high-pressure rotor blade caused by the presence of neighboring blade rows is investigated, with the individual effects of wake, shock and potential field interaction being determined. Two test geometries are considered: first, a h...

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Veröffentlicht in:	Journal of turbomachinery 2003-01, Vol.125 (1), p.33-39
Hauptverfasser:	Miller, R. J, Moss, R. W, Ainsworth, R. W, Harvey, N. W
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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