Characterizing Flow Effects of Ported Shroud Casing Treatment on Centrifugal Compressor Performance
Author:
Affiliation:
1. Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, Cambridge, MA 02139 e-mail:
2. Honeywell Turbo Technologies, Torrance, CA 90504 e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4035664/6307504/turbo_139_08_081005.pdf
Reference20 articles.
1. Application of Map Width Enhancement Devices to Turbocharger Compressor Stages,1988
2. Development of Wide Flow Range Compressor With Variable Inlet Guide Vane;R&D Rev. Toyota CRDL,2006
3. Numerical Fluid Analysis of a Variable Geometry Compressor for Use in a Turbocharger;R&D Rev. Toyota CRDL,2006
4. Numerical and Experimental Investigation of a Centrifugal Compressor With an Inducer Casing Bleed System;Proc. Inst. Mech. Eng., Part A,2001
5. Meanline Modeling of Ported Shroud Centrifugal Compressors,2012
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1. A New Unsteady Flow Control Technology of Centrifugal Compressor Based on Negative Circulation Concept;International Journal of Aerospace Engineering;2023-10-09
2. Flow Control Methods and Their Applicability in Low-Reynolds-Number Centrifugal Compressors—A Review;International Journal of Turbomachinery, Propulsion and Power;2017-12-29
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