TY - JOUR
T1 - Nonlinear model-order reduction for compressible flow solvers using the Discrete Empirical Interpolation Method
AU - Fosas de Pando, Miguel
AU - Schmid, Peter J.
AU - Sipp, Denis
N1 - Generated from Scopus record by KAUST IRTS on 2022-09-13
PY - 2016/11/1
Y1 - 2016/11/1
N2 - Nonlinear model reduction for large-scale flows is an essential component in many fluid applications such as flow control, optimization, parameter space exploration and statistical analysis. In this article, we generalize the POD–DEIM method, introduced by Chaturantabut & Sorensen [1], to address nonlocal nonlinearities in the equations without loss of performance or efficiency. The nonlinear terms are represented by nested DEIM-approximations using multiple expansion bases based on the Proper Orthogonal Decomposition. These extensions are imperative, for example, for applications of the POD–DEIM method to large-scale compressible flows. The efficient implementation of the presented model-reduction technique follows our earlier work [2] on linearized and adjoint analyses and takes advantage of the modular structure of our compressible flow solver. The efficacy of the nonlinear model-reduction technique is demonstrated to the flow around an airfoil and its acoustic footprint. We could obtain an accurate and robust low-dimensional model that captures the main features of the full flow.
AB - Nonlinear model reduction for large-scale flows is an essential component in many fluid applications such as flow control, optimization, parameter space exploration and statistical analysis. In this article, we generalize the POD–DEIM method, introduced by Chaturantabut & Sorensen [1], to address nonlocal nonlinearities in the equations without loss of performance or efficiency. The nonlinear terms are represented by nested DEIM-approximations using multiple expansion bases based on the Proper Orthogonal Decomposition. These extensions are imperative, for example, for applications of the POD–DEIM method to large-scale compressible flows. The efficient implementation of the presented model-reduction technique follows our earlier work [2] on linearized and adjoint analyses and takes advantage of the modular structure of our compressible flow solver. The efficacy of the nonlinear model-reduction technique is demonstrated to the flow around an airfoil and its acoustic footprint. We could obtain an accurate and robust low-dimensional model that captures the main features of the full flow.
UR - https://linkinghub.elsevier.com/retrieve/pii/S0021999116303448
UR - http://www.scopus.com/inward/record.url?scp=84982162695&partnerID=8YFLogxK
U2 - 10.1016/j.jcp.2016.08.004
DO - 10.1016/j.jcp.2016.08.004
M3 - Article
SN - 1090-2716
VL - 324
SP - 194
EP - 209
JO - Journal of Computational Physics
JF - Journal of Computational Physics
ER -