Minimal subspace rotation on the Stiefel manifold for stabilization and enhancement of projection-based reduced order models for the compressible Navier-Stokes equations
被引:54
作者:
Balajewicz, Maciej
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机构:
Univ Illinois, Dept Aerosp Engn, Urbana, IL 61801 USAUniv Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA
Balajewicz, Maciej
[1
]
Tezaur, Irina
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机构:
Sandia Natl Labs, Quantitat Modeling & Anal Dept, POB 969,MS 9159, Livermore, CA USAUniv Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA
Tezaur, Irina
[2
]
Dowell, Earl
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Duke Univ, Dept Mech Engn & Mat Sci, Durham, NC USAUniv Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA
Dowell, Earl
[3
]
机构:
[1] Univ Illinois, Dept Aerosp Engn, Urbana, IL 61801 USA
[2] Sandia Natl Labs, Quantitat Modeling & Anal Dept, POB 969,MS 9159, Livermore, CA USA
[3] Duke Univ, Dept Mech Engn & Mat Sci, Durham, NC USA
For a projection-based reduced order model (ROM) of a fluid flow to be stable and accurate, the dynamics of the truncated subspace must be taken into account. This paper proposes an approach for stabilizing and enhancing projection-based fluid ROMs in which truncated modes are accounted for a priori via a minimal rotation of the projection subspace. Attention is focused on the full non-linear compressible Navier-Stokes equations in specific volume form as a step toward a more general formulation for problems with generic non-linearities. Unlike traditional approaches, no empirical turbulence modeling terms are required, and consistency between the ROM and the Navier-Stokes equation from which the ROM is derived is maintained. Mathematically, the approach is formulated as a trace minimization problem on the Stiefel manifold. The reproductive as well as predictive capabilities of the method are evaluated on several compressible flow problems, including a problem involving laminar flow over an airfoil with a high angle of attack, and a channel-driven cavity flow problem. (C) 2016 Elsevier Inc. All rights reserved.
机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Amsallem, David
;
Farhat, Charbel
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机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Stanford Univ, Dept Mech Engn, Stanford, CA 94305 USA
Stanford Univ, Inst Computat & Math Engn, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Balajewicz, Maciej
;
Farhat, Charbel
论文数: 0引用数: 0
h-index: 0
机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Stanford Univ, Dept Mech Engn, Stanford, CA 94305 USA
Stanford Univ, Inst Computat & Math Engn, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Amsallem, David
;
Farhat, Charbel
论文数: 0引用数: 0
h-index: 0
机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Stanford Univ, Dept Mech Engn, Stanford, CA 94305 USA
Stanford Univ, Inst Computat & Math Engn, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Balajewicz, Maciej
;
Farhat, Charbel
论文数: 0引用数: 0
h-index: 0
机构:
Stanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA
Stanford Univ, Dept Mech Engn, Stanford, CA 94305 USA
Stanford Univ, Inst Computat & Math Engn, Stanford, CA 94305 USAStanford Univ, Dept Aeronaut & Astronaut, Stanford, CA 94305 USA