52nd Aerospace Sciences Meeting 2014
DOI: 10.2514/6.2014-1436
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The Use of Dynamic Basis Functions in Proper Orthogonal Decomposition

Abstract: Currently, the usefulness of proper orthogonal decomposition (POD) is limited to computational domains with fixed meshes and fixed boundaries. This paper presents a new POD method that enables the modeling of flow through computational domains with deforming meshes and/or moving boundaries. To achieve this goal, the solution is approximated using basis functions which, although not explicitly functions of time, depend on parameters associated with flow unsteadiness. Results are shown for transonic flow through… Show more

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Cited by 2 publications
(4 citation statements)
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“…where f k, c ( t ) is the nominal value of f k ( t ); n-degree space vector ˜ f k,s ( t ) is the basis function which can be obtained via the proper orthogonal decomposition (POD) method [26,27] or other identification methods [28,29] , and ˜ f k,s ( t ) also represents a basic form of uncertain loads or uncontrolled loads such as the harmonic disturbance; p k denotes the number of uncertain loads. b k, s , s = 1, …, p k is the uncertain parameter with respect to controlled load ˜ f k,s .…”
Section: Problem Statement and Mathematical Modelingmentioning
confidence: 99%
“…where f k, c ( t ) is the nominal value of f k ( t ); n-degree space vector ˜ f k,s ( t ) is the basis function which can be obtained via the proper orthogonal decomposition (POD) method [26,27] or other identification methods [28,29] , and ˜ f k,s ( t ) also represents a basic form of uncertain loads or uncontrolled loads such as the harmonic disturbance; p k denotes the number of uncertain loads. b k, s , s = 1, …, p k is the uncertain parameter with respect to controlled load ˜ f k,s .…”
Section: Problem Statement and Mathematical Modelingmentioning
confidence: 99%
“…The value of the artificial dissipation parameter νii was found using an energy-based stability analysis. Therefore, artificial dissipation was added to (16) to yield ȧ = F F F(a) + ν ν νS − τ τ τK.…”
Section: Artificial Dissipationmentioning
confidence: 99%
“…Both ζ and u displayed similar results. The time coefficients were calculated in three ways: (1) the line corresponding to "FOM" solved (6) for the "exact" time coefficients, (2) the line corresponding to "ROM with no BC" solved (15) for the time coefficients, and (3) the line corresponding to "ROM with BC" solved (16) for the time coefficients. Both ROM solutions were extrapolated past the sampling time of the FOM.…”
Section: Quasi-one-dimensional Nozzle Flowmentioning
confidence: 99%
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