A Generic Approach for Gas Turbine Adaptive Modeling
Author:
Affiliation:
1. SKF/Delta Consult, Kapelle, The Netherlands
2. National Aerospace Laboratory, NLR, Amsterdam, The Netherlands
3. Delft University of Technology, Delft, The Netherlands
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/128/1/13/5707800/13_1.pdf
Reference28 articles.
1. Doel, D. L. , 1992, “Temper—A Gas Path Analysis Tool for Commercial Jet Engines,” ASME Paper No. 92-GT-315.
2. Urban, L. A. , 1972, “Gas Path Analysis Applied to Turbine Engine Condition Monitoring,” AIAA Paper No. 72-1082.
3. Kamboukos, Ph., and Mathioudakis, K., 2003, “Comparison of Linear and Non-Linear Gas Turbine Performance Diagnostics,” ASME GT-2003-38518.
4. Stamatis, A., Mathioudakis, K., and Papailiou, K., 1989, “Adaptive Simulation of Gas Turbine Performance,” ASME Paper No. 89-GT-205.
5. Adaptive Modeling of Jet Engine Performance With Application of Condition Monitoring;Lambiris;J. Propul. Power
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