Modeling and Quantification of Model-Form Uncertainties in Eigenvalue Computations Using a Stochastic Reduced Model

被引:25
作者
Farhat, Charbel [1 ]
Bos, Adrien [2 ]
Avery, Philip [2 ,3 ]
Soize, Christian [4 ]
机构
[1] Stanford Univ, Dept Aeronaut & Astronaut, Aircraft Struct, William F Durand Bldg Room 257, Stanford, CA 94305 USA
[2] Stanford Univ, Dept Aeronaut & Astronaut, William F Durand Bldg Room 028, Stanford, CA 94305 USA
[3] US Army, Res Lab, Adelphi, MD 20783 USA
[4] Univ Paris Est, CNRS, Lab Modelisat & Simulat Multi Echelle, MSME UMR 8208, 5 Bd Descartes, F-77454 Marne La Vallee, France
关键词
ELEMENT DYNAMIC-MODELS; REDUCTION;
D O I
10.2514/1.J056314
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A feasible, nonparametric, probabilistic approach for modeling and quantifying model-form uncertainties associated with a computational model designed for the solution of a generalized eigenvalue problem is presented. It is based on the construction of a stochastic, projection-based reduced-order model associated with a high-dimensional model using three innovative ideas: 1) the substitution of the deterministic reduced-order basis with a stochastic counterpart featuring a reduced number of hyperparameters, 2) the construction of this stochastic reduced-order basis on a subset of a compact Stiefel manifold to guarantee the linear independence of its column vectors and the satisfaction of any constraints of interest, and 3) the formulation and solution of a reduced-order inverse statistical problem to determine the hyperparameters so that the mean value and statistical fluctuations of the eigenvalues predicted using the stochastic, projection-based reduced-order model match target values obtained from available data. Consequently, the proposed approach for modeling model-form uncertainties can be interpreted as an effective approach for extracting from data fundamental information and/or knowledge that are not captured by a deterministic computational model, and incorporating them in this model. Its potential for quantifying model-form uncertainties in generalized eigencomputations is demonstrated for a natural vibration analysis of a small-scale replica of an X-56-type aircraft made of a composite material for which ground-vibration-test data are available.
引用
收藏
页码:1198 / 1210
页数:13
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