Numerical and Experimental Comparison of a Tandem and Single Vane Deswirler Used in an Aero Engine Centrifugal Compressor

The present work is part of the research project at the Institute of Jet Propulsion and Turbomachinery at the RWTH Aachen University in collaboration with GE Aviation. The subject is the numerical and experimental analysis of two blading strategies used in the diffusion system of an aero engine cent...

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Veröffentlicht in:	Journal of turbomachinery 2014-04, Vol.136 (4), p.1-10
Hauptverfasser:	Wilkosz, Benjamin, Schmidt, Johannes, Guenther, Christian, Schwarz, Philipp, Jeschke, Peter, Smythe, Caitlin
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerospace engines Centrifugal compressors Design engineering Strategy Tandem configuration Three dimensional Vanes Walls
Online-Zugang:	Volltext
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