The Effects of Reynolds Number on the Efficiency of Centrifugal Compressor Stages
Author:
Affiliation:
1. Head Radial Compressor Development Group, Thermal Turbomachinery Division, Sulzer-Escher Wyss, Ltd., Zurich, Switzerland
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/107/2/541/5704477/541_1.pdf
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