This paper provides a comparative study on accuracy and efficiency of metamodels constructed from large datasets. Two examples inspired by large industrial applications are used to identify the best metamodeling technique. Artificial Neural Networks, Radial Basis Functions, Gaussian Process and Nonlinear regression are used to build metamodels. The examples used showcase a broad range of industrial applications in aircraft engines and gas turbines. Although Radial Basis Functions and Gaussian Process models are robust for small data sets, their high computational cost for large datasets reduces their practical application. ANN models are found to perform optimally when large number of training points are readily available and the accuracy requirements are high.
Skip Nav Destination
ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition
June 6–10, 2011
Vancouver, British Columbia, Canada
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-5466-2
PROCEEDINGS PAPER
A Comparative Study on Accuracy and Efficiency of Metamodels for Large Industrial Datasets
Arun K. Subramaniyan,
Arun K. Subramaniyan
GE Global Research, Niskayuna, NY
Search for other works by this author on:
Liping Wang,
Liping Wang
GE Global Research, Niskayuna, NY
Search for other works by this author on:
Randall Cepress
Randall Cepress
GE Aviation, Cincinnati, OH
Search for other works by this author on:
Arun K. Subramaniyan
GE Global Research, Niskayuna, NY
Liping Wang
GE Global Research, Niskayuna, NY
Don Beeson
GE Aviation, Cincinnati, OH
John Nelson
GE Aviation, Cincinnati, OH
Richard Berg
GE Aviation, Cincinnati, OH
Randall Cepress
GE Aviation, Cincinnati, OH
Paper No:
GT2011-46610, pp. 759-769; 11 pages
Published Online:
May 3, 2012
Citation
Subramaniyan, AK, Wang, L, Beeson, D, Nelson, J, Berg, R, & Cepress, R. "A Comparative Study on Accuracy and Efficiency of Metamodels for Large Industrial Datasets." Proceedings of the ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition. Volume 6: Structures and Dynamics, Parts A and B. Vancouver, British Columbia, Canada. June 6–10, 2011. pp. 759-769. ASME. https://doi.org/10.1115/GT2011-46610
Download citation file:
3
Views
0
Citations
Related Proceedings Papers
Related Articles
Degradation Modeling and Remaining Useful Life Prediction of Aircraft Engines Using Ensemble Learning
J. Eng. Gas Turbines Power (April,2019)
Empirical Tuning of an On-Board Gas Turbine Engine Model for Real-Time Module Performance Estimation
J. Eng. Gas Turbines Power (March,2008)
Artificial Intelligence for the Diagnostics of Gas Turbines—Part I: Neural Network Approach
J. Eng. Gas Turbines Power (July,2007)
Related Chapters
Modeling Technique of Product Master Model for Aero Engine Multidisciplinary Collaborative Design and Simulation
Proceedings of the 2010 International Conference on Mechanical, Industrial, and Manufacturing Technologies (MIMT 2010)
Method and Software of Technical Risk Assessment for a Civil Aero-Engine
Proceedings of the International Conference on Technology Management and Innovation
The Application of Computer Measurement and Control Technology in a Tester for Single-Jet Nozzles of Aero Engine
Proceedings of the International Conference on Technology Management and Innovation