Compressor Efficiency Variation With Rotor Tip Gap From Vanishing to Large Clearance
Author:
Affiliation:
1. e-mail:
2. e-mail: MIT Gas Turbine Laboratory, Cambridge, MA 02139
3. Siemens Energy, Inc., Orlando, FL 32828 e-mail:
4. Siemens AG, Mülheim an der Ruhr, 45473Germany e-mail:
5. Siemens Energy, Inc., Orlando, FL 32828 e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4007547/6296645/turb_135_3_031030.pdf
Reference28 articles.
1. Loss Sources and Magnitudes in Axial-Flow Compressors;ASME J. Eng. Power,1976
2. Experimental Study of a High-Throughflow Transonic Axial Compressor Stage;ASME J. Eng. Gas Turbines Power,1984
3. Experiments and Computations on Large Tip Clearance Effects in a Linear Cascade;ASME J. Turbomach.,2010
4. Effects of Upstream Rotor Vortical Disturbances on Time-Average Performance of Axial Compressor Stator: Part 1—Framework of Technical Approach and Rotor Wakes-Stator Blade Interactions;ASME J. Turbomach.,1999
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