Study of Near-Stall Flow Behavior in a Modern Transonic Fan With Compound Sweep
Author:
Affiliation:
1. NASA Glenn Research Center MS 5–11, 21000 Brookpark Road,Cleveland, OH 44135
2. Aero Technology Lab, GE Aviation, 1 Neumann Way,Cincinnati, OH 45215
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/fluidsengineering/article-pdf/doi/10.1115/1.4006878/5556460/071101_1.pdf
Reference16 articles.
1. A Numerical Modeling of Endwall and Tip-Clearance Flow of an Isolated Compressor;Hah;ASME J. Eng. Gas Turbines Power
2. The Effects of Tip Clearance on a Swept Transonic Compressor Rotor;Copenhaver;ASME J. Turbomach.
3. Tip Leakage Flow in Axial Compressors;Storer;ASME Journal Turbomach.
4. Suder, K. L., and Celestina, M. L., 1994, “Experimental and Computational Investigation of the Tip Clearance Flow in a Transonic Axial Compressor Rotor,” NASA TM-106711.
5. Recommendations for Achieving Accurate Numerical Simulation of the Tip Clearance Flows in Transonic Compressor Rotors;Van Zante;ASME J. Turbomach.
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