2006
DOI: 10.1016/j.jcp.2006.03.038
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Uncertainty quantification of limit-cycle oscillations

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Cited by 105 publications
(49 citation statements)
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“…In the following sections, a one-dimensional and a two-dimensional uniformly distributed random input ξ will be considered, where v (1) (ξ) and v (2) (ξ) will be defined later according to the numerical examples. For the outflow boundary condition at Γ o ⊂ ∂D socalled do-nothing boundary conditions are applied [12].…”
Section: The Algorithmmentioning
confidence: 99%
See 1 more Smart Citation
“…In the following sections, a one-dimensional and a two-dimensional uniformly distributed random input ξ will be considered, where v (1) (ξ) and v (2) (ξ) will be defined later according to the numerical examples. For the outflow boundary condition at Γ o ⊂ ∂D socalled do-nothing boundary conditions are applied [12].…”
Section: The Algorithmmentioning
confidence: 99%
“…In [29] a multielement approach was introduced, which is able to postpone the point of convergence breakdown to later simulation times based on a domain decomposition of the probability space. In [2] a similar idea was developed employing a wavelet multiresolution analysis [17,19], which, however, also suffers from the same drawback regarding the long term integration convergence breakdown. Recently, a time-dependent basis for capturing the time evolution of the probability distribution of the solution was introduced in [8,25].…”
mentioning
confidence: 99%
“…12 Other unsteady applications can also be found in literature. 2,13 In this paper, an efficient alternative approach for uncertainty quantification in oscillatory problems is proposed.…”
Section: Introductionmentioning
confidence: 99%
“…However, such approaches become impractical when each sample realization results from high-fidelity computational fluid and structural dynamics tools. Probabilistic collocation methodologies are promising candidates to get more insights into physical mechanisms of flutter and LCO [1,2] with affordable computational cost [3][4][5]. These studies are generally based on the use of ad hoc inviscid linear aerodynamics, and the stochastic response of the system is governed by the uncertainties associated with the nonlinear structural stiffness coefficients [5,6].…”
mentioning
confidence: 99%