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      Common Proper Orthogonal Decomposition-Based Spatiotemporal Emulator for Design Exploration

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          Abstract

          The present study develops a data-driven framework trained with high-fidelity simulation results to facilitate decision making for combustor designs. Its core is a surrogate model employing a machine-learning technique called kriging, which is uniquely combined with data-driven basis functions to extract and model the coherent structures underlying the flow dynamics. This emulation framework encompasses a sensitivity analysis of key design attributes, physics-guided classification of design parameter sets, and flow evolution modeling for a efficient design survey. A sensitivity analysis using Sobol indices and a decision tree is incorporated into the framework to better inform the model. The novelty of the proposed approach is the construction of the model through common proper orthogonal decomposition, allowing for data reduction and extraction of common coherent structures. As a specific example, the spatiotemporal evolution of the flowfields in swirl injectors is considered. The prediction accuracy of the mean flow features for new swirl injector designs is assessed, and the flow dynamics is captured in the form of power spectrum densities. The framework also demonstrates the uncertainty quantification of predictions, providing a metric for model fit. The significantly reduced computation time required for evaluating new design points enables an efficient survey of the design space.

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          Most cited references59

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          A Survey of Projection-Based Model Reduction Methods for Parametric Dynamical Systems

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            Reynolds averaged turbulence modelling using deep neural networks with embedded invariance

            There exists significant demand for improved Reynolds-averaged Navier–Stokes (RANS) turbulence models that are informed by and can represent a richer set of turbulence physics. This paper presents a method of using deep neural networks to learn a model for the Reynolds stress anisotropy tensor from high-fidelity simulation data. A novel neural network architecture is proposed which uses a multiplicative layer with an invariant tensor basis to embed Galilean invariance into the predicted anisotropy tensor. It is demonstrated that this neural network architecture provides improved prediction accuracy compared with a generic neural network architecture that does not embed this invariance property. The Reynolds stress anisotropy predictions of this invariant neural network are propagated through to the velocity field for two test cases. For both test cases, significant improvement versus baseline RANS linear eddy viscosity and nonlinear eddy viscosity models is demonstrated.
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              MODEL REDUCTION FOR FLUIDS, USING BALANCED PROPER ORTHOGONAL DECOMPOSITION

              C Rowley (2005)
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                Author and article information

                Journal
                aiaaj
                AIAA Journal
                AIAA Journal
                American Institute of Aeronautics and Astronautics
                0001-1452
                1533-385X
                30 April 2018
                June 2018
                : 56
                : 6
                : 2429-2442
                Affiliations
                Georgia Institute of Technology , Atlanta, Georgia 30332
                Author notes
                [*]

                Graduate Student, School of Aerospace Engineering.

                [†]

                Research Engineer, School of Aerospace Engineering; xingjian.wang@ 123456gatech.edu (Corresponding Author).

                [‡]

                Graduate Student, School of Industrial and Systems Engineering.

                [§]

                Research Engineer, School of Aerospace Engineering.

                [¶]

                Professor and Coca-Cola Chair in Engineering Statistics, School of Industrial and Systems Engineering.

                [**]

                William R. T. Oakes Professor and Chair, School of Aerospace Engineering.

                Article
                J056640 J056640
                10.2514/1.J056640
                bfed6ea6-0528-47c0-9c11-0f66ca2f6d6c
                Copyright © 2018 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp.
                History
                : 11 September 2017
                : 8 January 2018
                : 21 February 2018
                Page count
                Figures: 23, Tables: 6
                Funding
                Funded by: Coca-Cola Endowment
                Funded by: William R. T. Oakes Endowment
                Categories
                Regular Article

                Engineering,Physics,Mechanical engineering,Space Physics
                Engineering, Physics, Mechanical engineering, Space Physics

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