Experimental Investigation of Tip Clearance Flow in a Transonic Compressor With and Without Plasma Actuators
Author:
Affiliation:
1. GE Global Research, Niskayuna, NY 12309 e-mail:
2. AFRL/RQTT, Wright-Patterson AFB, OH 45433 e-mail:
3. Fellow ASME GE Aviation, Cincinnati, OH 45215 e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4028444/6301329/turbo_137_04_041008.pdf
Reference19 articles.
1. Suder, K. L., and Celestina, M. L., 1994, “Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor,” 39th International Gas Turbine and Aeroengine Congress and Exposition, The Hague, The Netherlands, June 13–16, Paper No. NASA-TM-106711.
2. Experimental and Computational Investigation of Stepped Tip Gap Effects on the Flowfield of a Transonic Axial-Flow Compressor Rotor;ASME J. Turbomach.,1998
3. The Effect of Tip Clearance on a Swept Transonic Compressor Rotor;ASME J. Turbomach.,1996
4. Numerical Investigation of Tip Clearance Effects in an Axial Transonic Compressor;J. Therm. Sci.,2012
5. Study of Casing Treatment Stall Margin Improvement Phenomena,1974
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