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Application of an Affine Nonlinear Galerkin Reduced-order Model to Compressible Fluid FlowsGalerkin reduced-order models (ROMs) often struggle to accurately capture multiscale fluid physics in challenging flow regimes such as flows experiencing compressibility effects. This in part stems from the global nature of both the basis construction problem and the spectral formulation itself. In this work, a multi-basis ROM is developed in an affine space based on proper orthogonal decomposition (POD) by projecting the full Navier-Stokes equations expressed in terms of the specific volume, velocity, and pressure primitive variables. The model is applied to high-fidelity numerical simulation datasets obtained for a canonical compressible flow configuration: the flow over a backward facing step at different subsonic Mach numbers. It is observed that application of an eigenvalue reassignment (ER) stabilization method is required to avoid early divergence of the ROM predictions for this configuration in the three Mach numbers tested. The sensitivity of the POD-ROM results to the choice of parameters in the stabilization algorithm is discussed.
Document ID
20220017776
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Donya Ramezanian
(University of Southern California Los Angeles, California, United States)
Michael W Lee
(Langley Research Center Hampton, Virginia, United States)
Ivan Bermejo-Moreno
(University of Southern California Los Angeles, California, United States)
Date Acquired
November 24, 2022
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: National Harbor, MD
Country: US
Start Date: January 23, 2023
End Date: January 27, 2023
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
WBS: 255421.04.07.21.01
CONTRACT_GRANT: 80LARC21CA002
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
Single Expert
Keywords
reduced-order model
proper orthogonal decomposition
compressible flow
shock wave boundary layer interaction
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