Using Shock Control Bumps to Improve Transonic Fan/Compressor Blade Performance
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Sheffield, Sheffield S1 3JD, UK e-mail:
2. Rolls-Royce, Derby DE24 8BJ, UK e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4042891/6421077/turbo_141_8_081003.pdf
Reference29 articles.
1. The Design of an Advanced Civil Fan Rotor;Ginder;ASME J. Turbomach.,1987
2. Three-Dimensional Shock Structures for Transonic/Supersonic Compressor Rotors;Prince;J. Aircraft,1980
3. Novel Compressor Blade Shaping Through a Free-Form Method;John;ASME J. Turbomach.,2017
4. Theoretical Aspects of Dromedaryfoil;Tai,1977
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