2018
DOI: 10.1142/s2591728518500226
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Quantification of Numerical Damping in the Acoustic Boundary Element Method for Two-Dimensional Duct Problems

Abstract: Spurious numerical damping in the collocation boundary element method is considered for plane sound waves in two-dimensional ducts subjected to rigid and absorbing boundary conditions. Its extent is quantified in both conditions based on a damping model with exponential decay, and meshes of linear and quadratic continuous elements are studied. An exponential increase of numerical damping with respect to frequency is found and the results suggest an upper bound for given element-to-wavelength ratios. The quanti… Show more

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Cited by 13 publications
(13 citation statements)
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References 25 publications
(27 reference statements)
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“…It is considered that real eigenvaulues are shifted into the complex plane following discretisation. This phenomenon is termed numerical damping [116][117][118][119].…”
Section: The Boundary Element Methods For the Generalised Boundary Conmentioning
confidence: 99%
“…It is considered that real eigenvaulues are shifted into the complex plane following discretisation. This phenomenon is termed numerical damping [116][117][118][119].…”
Section: The Boundary Element Methods For the Generalised Boundary Conmentioning
confidence: 99%
“…for x ∈ Ω j . Here, G j denotes the Green's function with the wavenumber of the respective region, that is, G j (x, y) = e k j |x−y| 4 |x − y| for x, y ∈ Ω j and x ≠ y (8) for j = 0, 1, 2, … , where denotes the complex unit. The boundary integral operators that map from one interface Γ n to another or the same interface Γ m are given by…”
Section: Boundary Integral Operatorsmentioning
confidence: 99%
“…This problem is often used in the computational acoustics community for benchmarking purposes 43 and extensive studies on associated discretization errors with respect to mesh sizes and element types are available in the literature. 44,45 The acoustic field is discretized using a uniform mesh of 1120 quadrilateral boundary elements with bilinear discontinuous sound pressure interpolation yielding 4480 degrees of freedom. We are interested in solving the resultant linear system (2) in the frequency range from 40 to 210 Hz with frequency steps of Δf = 1 Hz, ie, m = 171.…”
Section: Plane Sound Wave In a Closed Rigid Ductmentioning
confidence: 99%
“…The system is free of dissipation, and hence, resonances occur at the integer multiples of 50 Hz. This problem is often used in the computational acoustics community for benchmarking purposes and extensive studies on associated discretization errors with respect to mesh sizes and element types are available in the literature …”
Section: Numerical Examplesmentioning
confidence: 99%