Improved Perfectly Matched Layers for Acoustic Radiation and Scattering Problems

Similar documents
Computational Acoustic Attenuation Performance of Helicoidal Resonators Comparable to Experiment

The directivity of the forced radiation of sound from panels and openings including the shadow zone

Chapter 2 Introductory Concepts of Wave Propagation Analysis in Structures

Homogeneous and Inhomogeneous Model for Flow and Heat Transfer in Porous Materials as High Temperature Solar Air Receivers

POLYNOMIAL APPROXIMATIONS OF REGULAR AND SINGULAR VECTOR FIELDS WITH APPLICATIONS TO PROBLEMS OF ELECTROMAGNETICS

Prediction of Sound Propagation From Power Transmission Plant

A. G. Falkowski Chrysler Corporation, Detroit, Michigan 48227

Study on Characteristics of Sound Absorption of Underwater Visco-elastic Coated Compound Structures

Spectral Analysis by Stationary Time Series Modeling

SELF-SIMILAR FLOW UNDER THE ACTION OF MONOCHROMATIC RADIATION BEHIND A STRONG CYLINDRICAL SHOCK WAVE IN A NON-IDEAL GAS

CFD AS A DESIGN TOOL FOR FLUID POWER COMPONENTS

IMPACT MODELS AND COEFFICIENT OF RESTITUTION: A REVIEW

Uniformly best wavenumber approximations by spatial central difference operators: An initial investigation

On Gravity Waves on the Surface of Tangential Discontinuity

International Association of Scientific Innovation and Research (IASIR) (An Association Unifying the Sciences, Engineering, and Applied Research)

Roots Blower with Gradually Expanding Outlet Gap: Mathematical Modelling and Performance Simulation Yingjie Cai 1, a, Ligang Yao 2, b

Highly improved convergence of the coupled-wave method for TM polarization

Electromagnetic wave propagation. ELEC 041-Modeling and design of electromagnetic systems

VIBRATIONS OF SHALLOW SPHERICAL SHELLS AND GONGS: A COMPARATIVE STUDY

Lower bound solutions for bearing capacity of jointed rock

ME scope Application Note 16

NUMERICAL AND THEORETICAL INVESTIGATIONS ON DETONATION- INERT CONFINEMENT INTERACTIONS

Implementation and Validation of Finite Volume C++ Codes for Plane Stress Analysis

Optimal array pattern synthesis with desired magnitude response

A Quadratic Cumulative Production Model for the Material Balance of Abnormally-Pressured Gas Reservoirs

CFL Conditions for Runge-Kutta Discontinuous Galerkin Methods on Triangular Grids

Theoritical Analysis of Some Homogenized Metamaterials and Application of PML to Perform Cloaking and Back-scattering Invisibility

ANALYTIC APPROXIMATE SOLUTIONS FOR FLUID-FLOW IN THE PRESENCE OF HEAT AND MASS TRANSFER

Experimental acoustic identification of flow noise sources in expansion chambers

COMPARISON OF VARIOUS OPTIMIZATION TECHNIQUES FOR DESIGN FIR DIGITAL FILTERS

Calculation of gravity due to a vertical cylinder using a spherical harmonic series and numerical integration

Main Menu. Summary (1)

Paper C Exact Volume Balance Versus Exact Mass Balance in Compositional Reservoir Simulation

Minimax Design of Nonnegative Finite Impulse Response Filters

Preconditioning techniques for Newton s method for the incompressible Navier Stokes equations

1 University of Edinburgh, 2 British Geological Survey, 3 China University of Petroleum

Topology Optimization of Three Dimensional Structures under Self-weight and Inertial Forces

Estimation of the large covariance matrix with two-step monotone missing data

FastBEM Acoustics. Verification Manual , Advanced CAE Research, LLC (ACR) Cincinnati, Ohio, USA All Rights Reserved

FEM simulation of a crack propagation in a round bar under combined tension and torsion fatigue loading

4. Score normalization technical details We now discuss the technical details of the score normalization method.

Validation of Noise Footprint Calculation Model for a High Performance Military Aircraft

Seafloor Reflectivity A Test of an Inversion Technique

On the relationship between sound intensity and wave impedance

Churilova Maria Saint-Petersburg State Polytechnical University Department of Applied Mathematics

Lecture 2: Dispersion in Materials. 5 nm

HEAT TRANSFER IN STEADY-PERIODIC FLOWS OVER HEATED MICROWIRES

COMPARISON OF FREQUENCY DEPENDENT EQUIVALENT LINEAR ANALYSIS METHODS

3.4 Design Methods for Fractional Delay Allpass Filters

An Investigation on the Numerical Ill-conditioning of Hybrid State Estimators

r p = r o r cos( φ ) cos( α )

Time Domain Calculation of Vortex Induced Vibration of Long-Span Bridges by Using a Reduced-order Modeling Technique

Research Article A Wavelet Algorithm for Fourier-Bessel Transform Arising in Optics

ADVANCED SIGNAL PROCESSING METHODS FOR EVALUATION OF HARMONIC DISTORTION CAUSED BY DFIG WIND GENERATOR

Research of power plant parameter based on the Principal Component Analysis method

Speed of sound measurements in liquid Methane at cryogenic temperature and for pressure up to 10 MPa

Dispersion relation of surface plasmon wave propagating along a curved metal-dielectric interface

The role of current loop in harmonic generation from magnetic metamaterials in two polarizations

Radial Basis Function Networks: Algorithms

REFLECTION AND TRANSMISSION BAND STRUCTURES OF A ONE-DIMENSIONAL PERIODIC SYSTEM IN THE PRESENCE OF ABSORPTION

Using Gamma-Ray to Determine the Homogeneity of Some Building Materials

Algebraic Parameter Estimation of Damped Exponentials

Multistep variable methods for exact integration of perturbed stiff linear systems

P043 Anisotropic 2.5D - 3C Finite-difference Modeling

Finite Element Analysis of Acoustic Scattering

ME 375 System Modeling and Analysis. Homework 11 Solution. Out: 18 November 2011 Due: 30 November 2011 = + +

Analysis of Pressure Transient Response for an Injector under Hydraulic Stimulation at the Salak Geothermal Field, Indonesia

Prediction of the Excitation Force Based on the Dynamic Analysis for Flexible Model of a Powertrain

A Model for Randomly Correlated Deposition

Simple geometric interpretation of signal evolution in phase-sensitive fibre optic parametric amplifier

ACOUSTIC PREDICTIONS IN OFFSHORE PLATFORMS

The Numerical Simulation of Gas Turbine Inlet-Volute Flow Field

HENSEL S LEMMA KEITH CONRAD

dn i where we have used the Gibbs equation for the Gibbs energy and the definition of chemical potential

International Journal of Mathematics Trends and Technology- Volume3 Issue4-2012

Meshless Methods for Scientific Computing Final Project

Phase transition. Asaf Pe er Background

MODELING THE RELIABILITY OF C4ISR SYSTEMS HARDWARE/SOFTWARE COMPONENTS USING AN IMPROVED MARKOV MODEL

SEG Houston 2009 International Exposition and Annual Meeting

LINEAR SYSTEMS WITH POLYNOMIAL UNCERTAINTY STRUCTURE: STABILITY MARGINS AND CONTROL

Modelling of non-uniform DC driven glow discharge in argon gas

The individual electric and magnetic waves are in phase. The fields peak at the same position at the same time.

Convergence performance of the coupled-wave and the differential methods for thin gratings

A SIMPLE PLASTICITY MODEL FOR PREDICTING TRANSVERSE COMPOSITE RESPONSE AND FAILURE

Heat Transfer Analysis in the Cylinder of Reciprocating Compressor

AN APPROACH FOR THE MODEL BASED MONITORING OF PIEZOELECTRIC ACTUATORS

FE FORMULATIONS FOR PLASTICITY

Pressure-sensitivity Effects on Toughness Measurements of Compact Tension Specimens for Strain-hardening Solids

Parameters Optimization and Numerical Simulation for Soft Abrasive Flow Machining

Preliminary Uncertainty Estimation of the Pressure Distortion Coefficient of a Pressure. Balance by FEM Calculations

Magnetostrictive Dynamic Vibration Absorber (DVA) for Passive and Active Damping

Finite-State Verification or Model Checking. Finite State Verification (FSV) or Model Checking

Proceedings of Meetings on Acoustics

pp physics, RWTH, WS 2003/04, T.Hebbeker

EVALUATION OF THE THEORETICAL ERROR FOR THE LIGHTNING PEAK CURRENT AS MEASURED BY LIGHTNING LOCATION SYSTEMS

Positivity, local smoothing and Harnack inequalities for very fast diffusion equations

Optical Fibres - Dispersion Part 1

Numerical Simulation and Experimental of Residual Stress Field of SAE1070 Spring Steel Induced by Laster Shock

Di raction: Boundary Value Problems of Electromagnetic Waves

Continuous Steel Casting System Components

Transcription:

NATO Undersea Research Centre Partnering for Maritime Innovation Presented at the COMSOL Conference 008 Hannover Acoustics Session Wed 5 November 008, 13:00 15:40. Imroved Perfectly Matched Layers for Acoustic Radiation and Scattering Problems Mario Zamolli, *,1 Nils Malm, Alessandra Tesei 1 1 NURC NATO Research Centre, La Sezia (Italy) COMSOL AB, Stockholm (Sweden)

Overview The Sommerfeld Radiation Condition and Perfectly Matched Layers (PML s). Problems caused by the stee decay of evanescent waves at low frequencies. Imroved PML formulation: (i) Imroved accuracy in the resence of evanescent waves at low frequencies. (ii) Stability of the mesh with resect to frequency. Real-life alication: loudseaker design. Conclusions and further develoment.

The Sommerfeld Radiation Condition In an unbounded medium [ex(+i ω t), k= ω /c] : r + + k ik = = 0 1 o r Helmholtz equation describing the acoustic ressure., r In a comuter model, r must be finite. Sommerfeld radiation condition r source(s) and/or scatterer(s) exterior fluid The Sommerfeld condition must be aroximated numerically.

Perfectly Matched Layer (PML) An (efficient!) technique for aroximating the Sommerfeld BC. J.-P. Bérenger, A erfectly matched layer for the absortion of electromagnetic waves, Journal of Comutational Physics, Vol. 114,. 185 00 (1994). PML s Can be easily adated to CONVEX geometries:. Straightforward imlementation via comlex coordinate scaling. F. Collino, P. Monk, The erfectly matched layer in curvilinear coordinates, SIAM J. Sci. Comut., Vol. 19(6),. 061 090 (1998). F. Ihlenburg, Finite Element Analysis of Acoustic Scattering, Sringer-Verlag (1998). M. Zamolli, A. Tesei, F.B. Jensen, N. Malm, J.B. Blottman, J.Acoust.Soc.Am. 1, 147 1485 (007). z Fluid Domain (hysical) x PML (non-hysical) Perturbed Helmholtz Equation (PML): iω iω + + k = 0 iω + σ ( x) x ( ) iω + σ x x z Reflections are negligible. ~ x + z + k Comlex coordinate Daming only in the x-direction. = 0

PML Formulation in the Current Imlementation Fluid z (hysical) PML x PDE in the PML: ~ x + z + k = 0 D PML scaled coordinate: ~ x = (1 i) λ / Normalizing the scaled coordinate w.r.t. the wavelength λ no need to adjust the mesh density in the PML in x-direction as the frequency varies Mesh stability. The scaled coordinate is a olynomial, with equal ower n in the real art and in the imaginary art. ( x D) n The real and the imaginary art of the scaled coordinate each have different effects, deending on whether the incident wave is roagating or evanescent.

Effect of the Real and Imaginary Parts of the Scaling Wave Tye PML scaled coordinate Real Part Imaginary Part Proagating Evanescent Resolution of the oscillatory comonents in the PML, no daming. Daming (Decay) of the evanescent wave in the PML. Daming in the PML. Raidly growing imaginary art good daming. Surious anti-causal waves, which are absorbed by the PML. Problems at very low frequencies, where the evanescent field decays steely: the PML over-dams an already steely decaying wave PML accuracy roblems.

Imroved PML Scaling Fluid z (hysical) PML D x ( ) n ( x / D) r + i log 1 ( x / D ) i ~ x = Aλ n arameter ~0.5 sensitivity convergence n i ka 1 log, = 10 10 1, ka ka < 10 10 At high frequencies ka>10 : raidly growing log (1-x/D) scaling of the imaginary art good daming of roagating waves. At low frequencies: log (1-(x/D) ni ) with exonent of n i >1 in the imaginary art imaginary coordinate grows more slowly near the interface with the hysical domain, element size comressed near the interface, good resolution of the hase of the decaying wave.

Imroved PML Scaling Fluid z (hysical) PML D x ( ) n ( x / D) r + i log 1 ( x / D ) i ~ x = Aλ n n r 1 log10 = 1, ka, ka < 1 ka 1 At low frequencies : real art grows slowly near the boundary element size comressed near the interface, raidly decaying evanescent waves are better resolved by the PML near the interface with the hysical domain, imroved accuracy.

Examle: Circular Piston Radiation Sound-ressure level on axis, at 0.1a. PML COMSOL: 1 quadratic elements in the PML, old PML scaling. air rigid baffle rescribed constant normal velocity. Piston radius = a. Errors at low frequency in the solution with the old PML scaling.

Comarison: old vs Imroved Scaling Relative error vs. ka

Plane-wave Scattering from a Hard Shere Scattered ressure level on surface, backscatter. Relative error vs. ka

Helmholtz resonator Evanescent field at the oening. Performance of the Modified PML Cylindrical Sub-woofer Accurate solution with 4-layer modified PML, comared to 16-layer standard PML.

Audio Loudseaker Design SPL (db) Black: 8 Layer standard PML in Comsol Red: 1 Layer new PML. Freq. (Hz)

Conclusions and Further Develoment The real and imaginary arts of the PML coordinate scaling affect evanescent and roagating wave comonents in different ways. Modified scaling strategy roosed: (i) imroves the erformance at low frequencies, where evanescent waves dominate. (ii) mesh stability with resect to frequency, from ka = 1/100 to ka = 100. Increasing error at high frequencies observed in radiation roblems To be addressed. What is a in ka? Problem deendence? A measure of the smallest wave scales of the roblem?