Uncertainty Quantification Integrated with the Reduced-Dimensional Modeling of Supersonic Shear Flows
ORAL
Abstract
The authors present a novel approach where reduced-dimensional modeling leveraging K-means clustering [3] and uncertainty quantification has been integrated with reduced-order modeling. The approach is demonstrated by modeling the supersonic flow over a double-fin-on-cylinder test article [4] where shock-boundary layer interactions are dominant. Heterogeneous experimental data for 20-degree and 5-degree fins was used as the so-called training data to develop a reduced-order model of the surface pressure distribution for a fin with a 10-degree incident angle. Further, Reynolds averaged Navier Stokes (RANS) computational fluid dynamics (CFD) calculations are conducted for the same 10-degree configuration, and the results are leveraged as additional training data. The experimental data obtained from various facilities can have different dimensionality and CFD data can have different dimensionality depending upon the grid density and numerical methods employed. If the dimensionality of each dataset is reduced to the same dimensionality, all data can be fused and the resulting large dataset can be used to build the reduced-order model. The research challenges in performing this dimensionality reduction are (1) maintaining an acceptably accurate representation of the relevant physical interactions and (2) quantifying both the contribution of the error and imprecision in dimensionality reduction and uncertainty inherent in the training data to the uncertainty of a reduced-order model’s predictions. This research will show the results from dimensionality reduction and reduced-order modeling, and implement existing uncertainty quantification (UQ) methods that address the above research challenges.
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Publication: [1] Kuya, Y., Takeda, K., Zhang, X., and Forrester, A. I., "Multifidelity Surrogate Modeling of Experimental and Computational<br> Aerodynamic Data Sets," AIAA Journal, Vol. 49, No. 11, 2011, pp. 289–298. https://doi.org/10.2514/1.J050384.<br>[2] Brunton, S. L., Proctor, J. L., and Kutz, J. N., "Discovering governing equations from data by sparse identification of nonlinear dynamical systems," Proceedings of the National Academy of Sciences of the United States, CP849, Vol. 113, PNAS, 2016, pp. 3932–3937. https://doi.org/10.1073/pnas.1517384113.<br>[3] Scikit-learn: Machine Learning in Python, Pedregosa et al., JMLR 12, pp. 2825-2830, 2011.<br>[4] Cho, W., "Double-Fin Induced Shock Wave/Turbulent Boundary Layer Interactions over a Cylindrical Surface," Master's<br>thesis, North Carolina State University, 2020.
Presenters
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Kevin Hartman
University of Tennessee Space Institute
Authors
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Kevin Hartman
University of Tennessee Space Institute
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Ragini Acharya
University of Tennessee Space Institute