Experimental and Numerical Verification of an Optimization of a Fast Rotating High-Performance Radial Compressor Impeller
Author:
Affiliation:
1. Institute of Propulsion Technology, German Aerospace Center DLR, Linder Hoehe, Cologne 51147, Germany e-mail:
2. Institute of Propulsion Technology, German Aerospace Center DLR, Linder Hoehe, Cologne 51147, Germany
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4036357/6307348/turbo_139_10_101007.pdf
Reference12 articles.
1. Investigations of the Flow Through a High Pressure Ratio Centrifugal Impeller,2002
2. Flow Study of a Redesigned High Pressure Ratio Centrifugal Compressor;AIAA J.,2008
3. Automated Multidisciplinary Optimization of a Transonic Axial Compressor,2009
4. Multidisciplinary 3D-Optimization of a Fan Stage Performance Map With Consideration of the Static and Dynamic Rotor Mechanics,2010
5. Raitor, T., Reutter, O., Aulich, M., and Nicke, E., 2013, “Aerodynamic Design Studies of a Transonic Centrifugal Compressor Impeller Based on Automatic 3D-CFD Optimization,” 10th European Turbomachinery Conference, Lappeenranta, Finland, Apr. 15–19, Paper No. A082.
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