Journal article
J. Weinmeister, N. Xie, Xinfeng Gao, A. Prasad, Sourajeet Roy
2018
2018
Semantic Scholar
DOI
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APA
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Weinmeister, J., Xie, N., Gao, X., Prasad, A., & Roy, S. (2018). Analysis of a Polynomial Chaos-Kriging Metamodel for Uncertainty Quantification in Aerospace Applications.
Chicago/Turabian
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Weinmeister, J., N. Xie, Xinfeng Gao, A. Prasad, and Sourajeet Roy. “Analysis of a Polynomial Chaos-Kriging Metamodel for Uncertainty Quantification in Aerospace Applications” (2018).
MLA
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Weinmeister, J., et al. Analysis of a Polynomial Chaos-Kriging Metamodel for Uncertainty Quantification in Aerospace Applications. 2018.
BibTeX Click to copy
@article{j2018a,
title = {Analysis of a Polynomial Chaos-Kriging Metamodel for Uncertainty Quantification in Aerospace Applications},
year = {2018},
author = {Weinmeister, J. and Xie, N. and Gao, Xinfeng and Prasad, A. and Roy, Sourajeet}
}
Abstract
Metamodeling can be effective for uncertainty quantification in computational fluid dynamics simulations. In this research, we introduce modifications to our existing metamodel1 that combines a reduced polynomial chaos expansion approach and universal Kriging (RPCK) and evaluate the new metamodel for aerospace applications. Focus is given to determine which metamodel parameters most effect the solution accuracy by measuring the errors. Additionally, a new adaptive refinement algorithm is explored and the methodology is presented. Results show the metamodel’s need for robustness in aerospace engineering applications, including the non-smooth output of separated airflow.