Methodology and Validation of Surge Modeling in a Three-Shaft Compression System
Author:
Affiliation:
1. Imperial College London Department of Mechanical Engineering, , London SW7 2AZ , UK
2. Rolls-Royce plc , P.O. Box 31, Derby DE24 8BJ , UK
Abstract
Funder
Rolls-Royce
Publisher
ASME International
Subject
Mechanical Engineering
Link
https://asmedigitalcollection.asme.org/turbomachinery/article-pdf/145/12/121006/7051091/turbo_145_12_121006.pdf
Reference19 articles.
1. Rotating Stall Observations in a High Speed Compressor–Part I: Experimental Study;Dodds;ASME J. Turbomach.,2015
2. Rotating Stall Observations in a High Speed Compressor–Part II: Numerical Study;Dodds;ASME J. Turbomach.,2015
3. Numerical Simulation of Aerodynamic Instabilities in a Multistage High-Speed High-Pressure Compressor on Its Test Rig–Part II: Deep Surge;Crevel;ASME J. Turbomach.,2014
4. Numerical Analysis and Validation of the Rotor Blade Vibration Response Induced by High Pressure Compressor Deep Surge;Giersch,2014
5. Unsteady Flow and Aeroelasticity Behaviour of Aero-Engine Core Compressors During Rotating Stall and Surge;Vahdati;ASME. J. Turbomach.,2008
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