NASA HECC Geometry and Performance Review Part 3: A Numerical and Experimental Investigation of Tip Clearance Effects on the Vaneless Diffuser Configuration

Tip clearance effects in centrifugal compressors have been extensively investigated to understand the losses associated with the flow in the impeller tip clearance gap between the rotating blades and the stationary shroud. In Part 3 of this multipart investigation, experimental data and validated nu...

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Bibliographische Detailangaben

Hauptverfasser:	Harrison, Herbert M, Nguyen-Huynh, Tam, Mathison, Randall M
Format:	Other
Sprache:	eng
Schlagworte:	Aerodynamics
Online-Zugang:	Volltext bestellen
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