Radial Migration of Shed Vortices in a Transonic Rotor Following a Wake Generator: A Comparison Between Time Accurate and Average Passage Approaches
Author:
Affiliation:
1. University of Cincinnati
2. Brigham Young University
3. Air Force Research Laboratory, Wright-Patterson Air Force Base
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4001241/5613108/031018_1.pdf
Reference19 articles.
1. The Effects of Blade-Row Spacing on the Flow Capacity of a Transonic Rotor;Chriss
2. Analysis of a Highly Loaded, Transonic, Inlet Compressor Stage: Isolated and Multi-Stage Performance;Car
3. Gorrell, S. E. , 2001, “An Experimental and Numerical Investigation of Stator-Rotor Interactions in a Transonic Compressor,” Ph.D. thesis, Mechanical Engineering, Iowa State University, Ames, IA.
4. Stator-Rotor Interactions in a Transonic Compressor—Part 2: Description of a Loss-Producing Mechanism;Gorrell;ASME J. Turbomach.
5. Law, C. H., and Wennerstrom, A. J., 1989, “Two Axial Compressor Designs for a Stage Matching Investigations,” Paper No. AF-WAL-TR-89-2005.
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1. Investigation on shock-induced separation loss mitigation method considering radial equilibrium in a transonic compressor rotor;The Aeronautical Journal;2022-03-09
2. Analysis and Prediction of Shock-Induced Vortex Circulation in Transonic Compressors;Journal of Turbomachinery;2015-10-06
3. Particle Image Velocimetry Analysis on the Effect of Stator Loading on Transonic Blade-Row Interactions;Journal of Turbomachinery;2012-09-04
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