Effect of Ice and Blade Interaction Models on Compressor Stability
Author:
Affiliation:
1. GE Global Research Center, One Research Circle, Niskayuna, NY 12309 e-mail:
2. GE Global Research Center, One Research Circle, Niskayuna, NY 12309
3. GE Aviation, 1 Neumann Way, Evandale, OH 45215
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/doi/10.1115/1.4034983/6305354/turbo_139_04_041001.pdf
Reference23 articles.
1. The Ice Particle Threat to Engines in Flight,2006
2. Current Perspectives on Jet Engine Power Loss in Ice Crystal Conditions: Engine Icing,2009
3. Engine Icing Modeling and Simulation—Part 1: Ice Crystal Accretion on Compression System Components and Modeling Its Effects on Engine Performance,2011
4. Modeling of Ice Accretion and Shedding in Turbofan Engines With Mixed Phase/Glaciated (Ice Crystal) Conditions,2007
5. FENSAP-ICE: Ice Accretion in Multi-Stage Jet Engines,2009
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