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VISUALIZATION OF SOUND REFLECTION AND DIFFRACTION BY THE FINITE DIFFERENCE TIME DOMAIN METHOD Shinichi SAKAMOTO Institute of Industrial Science The University of Tokyo 4-6-1 Komaba, Meguro-ku, Tokyo, 153-8505 Japan E-mail: [email protected] Hideki TACHIBANA Department of Computer Science Chiba Institute of Technology E-mail: [email protected] ABSTRACT Visualization of sound field helps us to intuitively understand mechanisms of various acoustic phenomena. This report presents some examples of sound field visualization based on numerical analysis. In order to analyze such complicated acoustic phenomena as reflection, diffraction and interference, the finite difference time domain (FDTD) method is applied to the calculation. In the FDTD algorithm, all of sound field is computed in discrete time steps and therefore transient acoustic phenomena can be easily animated. As an application of the numerical technique to environmental noise control, sound reflection and diffraction under various geometrical conditions such as undulations of ground, several types of noise barriers, embankments, depressed/semi-underground road structures, etc. are introduced in this report. It should be added that the physical quantities such as sound pressure exposure level and sound intensity can be deduced from the calculation results and therefore the method is useful from engineering view point. KEYWORDS: Visualization, Sound reflection and diffraction, FDTD method INTRODUCTION To examine and understand such complicated acoustic phenomena as reflection, diffraction and interference, visualization of sound fields is very effective not only from an educational viewpoint but also from a practical engineering viewpoint in building acoustics and noise control engineering. Recently, such numerical analysis techniques as finite element method

VISUALIZATION OF SOUND REFLECTION AND ......FDTD algorithm, the sound pressure and particle velocity in a sound field are directly computed in discrete time steps and therefore transient

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  • VISUALIZATION OF SOUND REFLECTION AND DIFFRACTION BY THE FINITE DIFFERENCE TIME DOMAIN METHOD

    Shinichi SAKAMOTO

    Institute of Industrial Science The University of Tokyo

    4-6-1 Komaba, Meguro-ku, Tokyo, 153-8505 Japan E-mail: [email protected]

    Hideki TACHIBANA

    Department of Computer Science Chiba Institute of Technology

    E-mail: [email protected]

    ABSTRACT Visualization of sound field helps us to intuitively understand mechanisms of various acoustic phenomena. This report presents some examples of sound field visualization based on numerical analysis. In order to analyze such complicated acoustic phenomena as reflection, diffraction and interference, the finite difference time domain (FDTD) method is applied to the calculation. In the FDTD algorithm, all of sound field is computed in discrete time steps and therefore transient acoustic phenomena can be easily animated. As an application of the numerical technique to environmental noise control, sound reflection and diffraction under various geometrical conditions such as undulations of ground, several types of noise barriers, embankments, depressed/semi-underground road structures, etc. are introduced in this report. It should be added that the physical quantities such as sound pressure exposure level and sound intensity can be deduced from the calculation results and therefore the method is useful from engineering view point. KEYWORDS: Visualization, Sound reflection and diffraction, FDTD method

    INTRODUCTION

    To examine and understand such complicated acoustic phenomena as reflection, diffraction and interference, visualization of sound fields is very effective not only from an educational viewpoint but also from a practical engineering viewpoint in building acoustics and noise control engineering. Recently, such numerical analysis techniques as finite element method

  • (FEM) and boundary element method (BEM) have become popular in acoustics and they are often applied to the visualization of sound fields. Among these numerical methods, the authors have been investigating the application of the finite difference time domain (FDTD) method [1,2,3] to various problems in architectural acoustics and noise control engineering. In the FDTD algorithm, the sound pressure and particle velocity in a sound field are directly computed in discrete time steps and therefore transient acoustic phenomena can be easily animated. As an application of this numerical technique, some examples of visualization of sound reflection and diffraction around undulations of ground, several types of noise barriers and depressed/ semi-underground road structures are introduced in this report.

    THEORY The sound wave in a 2-dimensional sound field is described by the following differential equations. Equations (1) and (2) are the momentum equations in x- and y- directions, respectively, and Eq. (3) is the continuity equation.

    ( ) ( ) 0,,,, =∂

    ∂+

    ∂∂

    ttyxu

    xtyxp xρ (1)

    ( ) ( ) 0,,,, =∂

    ∂+

    ∂∂

    ttyxu

    ytyxp yρ (2)

    ( ) ( ) ( ) 0,,,,,, =⎟⎟⎠

    ⎞⎜⎜⎝

    ⎛∂

    ∂+

    ∂∂

    +∂

    ∂y

    tyxux

    tyxut

    tyxp yxκ (3)

    where, p is the sound pressure, ux and uy are the particle velocities in x- and y- directions, respectively, ρ is the density of the air and κ is the volume elastic modulus of the air.

    The spatial and time derivatives of an arbitrary function f, xf ∂∂ , yf ∂∂ and tf ∂∂ , can be approximated by the central finite difference forms as ( ) xxxfxxf ∆∆−−∆+ )2()2( , ( ) yyyfyyf ∆∆−−∆+ )2()2( and ( ) tttfttf ∆∆−−∆+ )2()2( , respectively. Here, ∆t is the discrete time step, and ∆x and ∆y are the spatial intervals. By adopting the staggered grid system with square-grids (∆x=∆y) as shown in Fig.1, the following equations are obtained for a discrete system.

    ( ) ( ) ( ) ( ){ }jipjiphtjiujiu nnnx

    nx ,,1,2/1,2/1

    21211 +++ −+∆∆

    −+=+ρ

    (4)

    ( ) ( ) ( ) ( ){ }jipjiphtjiujiu nnny

    ny ,1,2/1,2/1,

    21211 +++ −+∆∆

    −+=+ρ

    (5)

    ( ) ( ) ( ) ( ) ( ) ( )⎪⎭

    ⎪⎬⎫

    ⎪⎩

    ⎪⎨⎧

    −−++

    ∆−−+

    ∆−= −+h

    jiujiuh

    jiujiutjipjip

    ny

    ny

    nx

    nxnn 21,21,,21,21,, 2121 κ (6)

    where, ∆h is the size of the square-grid and indices n, n+1/2, n-1/2 and n+1 denote time steps. As the initial condition, a continuous distribution of sound pressure was set (see Fig.2).

    Several types of profiles of the initial sound pressure distribution are possible. Among them, following two types of profiles expressed by the following equations were adopted in this study.

  • ( ) ( )( )⎪⎩

    ⎪⎨⎧

    ∆>

  • Under the configuration of the impulse source and the barrier shown in Fig. 4, instantaneous sound pressure distribution in each time step was calculated and the sound propagation process was visualized. The snap shots of the sound pressure distribution for Types 1, 2 and 3 at every 16 ms are shown in Figures 5(a), 5(b) and 5(c), respectively. In these figures, the amplitude of sound pressure is shown by monochrome shade. In Fig.5(a) for Type 1 barrier, a simple pattern of sound diffraction at the top of the straight barrier is clearly seen. The diffraction sound makes a circular wave front of which amplitude varies according to the diffraction angle. On the other hand, in the cases of Type 2 and Type 3 barriers, the sound propagation is much more complicated. In these cases, multiple reflections occur inside the area between the overhang of the barrier and the road surface. These multiple reflections make secondary diffractions as shown in the figures of 48 ms and 64 ms.

    16 ms

    32 ms

    48 ms

    16 ms

    32 ms

    48 ms

    16 ms

    32 ms

    48 ms

    S S S16 ms

    32 ms

    48 ms

    16 ms

    32 ms

    48 ms

    16 ms

    32 ms

    48 ms

    16 ms

    32 ms

    48 ms

    16 ms

    32 ms

    48 ms

    16 ms

    32 ms

    48 ms

    S S S

    (a) Type 1 (b) Type 2 (c) Type 3

    Figure 5 Visualization of sound diffraction over noise barriers. Sound diffraction over embankment[7] The second example is sound diffraction over embankments. In assessment of noise attenuation by embankment, which is often used as

    (a) Type 1(Straight wall)

    H=5

    m

    H=5

    m

    W=3 m

    (b) Type 2(Arc wall)

    H=5

    m

    W=3 m

    (c) Type 3(Inverse-L wall)

    (a) Type 1(Straight wall)

    H=5

    m

    (a) Type 1(Straight wall)

    H=5

    mH

    =5 m

    H=5

    mH

    =5 m

    H=5

    m

    W=3 m

    (b) Type 2(Arc wall)

    H=5

    m

    W=3 m

    H=5

    m

    W=3 m

    (b) Type 2(Arc wall)

    H=5

    m

    W=3 m

    (c) Type 3(Inverse-L wall)

    H=5

    m

    W=3 m

    H=5

    m

    W=3 m

    (c) Type 3(Inverse-L wall)

    Rigid ground

    Sound absorbing layer

    50 m

    25m

    2.4 m

    2.4 m

    Barrier

    Sound source (Receiving point)10 m (15 m)10 m (15 m)

    Figure 3 Sectional shapes of barriers under investigation.

    Figure 4 Calculation domain for the FDTD method.

  • countermeasure against aircraft noise, the embankment is substituted by an equivalent straight barrier and diffraction chart derived by Maekawa is extendedly applied. The applicability of such usage of the chart, however, is not fully examined and therefore the authors made numerical investigation using the FDTD method. In this report, sound propagation around embankment is focused on and required outcome will be introduced.

    Figure 6 shows cross sectional shapes of barriers and an embankment under investigation- . Type 1 : thin wall, Type 2 : thick barrier and Type 3 : trapezoid embankment. Sound source was assumed to be at 10 m in front of the center of the barriers on a rigid ground. As an example of the calculation results, snap shots of transient sound pressure distribution at every 15 ms are shown in figure 7. In the case of thin wall (Type 1), sound diffraction at the top edge of the barrier is clearly seen. Circular wave front is generated at the edge as if secondary sound source were located at the point. In the case of thick wall, two diffracted waves are seen and amplitude of sound wave in the shadow area decrease. On the other hand in the case of embankment, sound wave proceeds along the slopes of the embankment and amplitude of the diffracted sound in the shadow area do not so much decrease.

    3 m3 m3 m 3 m

    2 m

    3 m

    2 m

    3 m

    2 m

    30°

    2 m

    30°

    2 m

    30°30°

    2 m2 m

    Type 1 Type 2 Type 3

    Figure 6 Sectional shape of embankments under investigation.

    Sound propagation from depressed/semi-underground road[8] In order to prevent noise propagation from highways, depressed or semi-underground structure is used sometimes. However, noise prediction method for this kind of road structures has not yet been established

    Figure 7 Sound propagation around barrier and embankment.

    Type 1 Type 2 Type 3

  • and therefore the authors are making a numerical investigation to develop a practical calculation method applicable to these road structures. From the results, some examples of sound field visualization are introduced here.

    The cross sections of the road structures under investigation and the sound source position are shown in Fig.8. These are (a) depressed road without sound absorption treatment, (b) the same one with absorption treatment on the sidewalls, (c) semi-underground road without sound absorption treatment and (d) the same one with absorption treatment on the sidewalls. As the condition of sound absorption treatment, 80% sound absorption coefficient was assumed over all frequencies. The instantaneous sound pressure distributions at every 50 ms after the emission of the impulse source are shown in each series of Figures 9 (a) to (d). As for the depressed structure, in the case where the sidewalls are assumed reflective shown in the series of Fig.9 (a), remarkable multiple reflections are seen between the sidewalls and strong sound waves caused by the multiple reflections propagate intermittently outside the road structure. On the other hand, in the case where the sidewalls are absorptive shown in the series of Fig. 9 (b), the multiple reflection is much reduced and consequently the subsequent reflections after the direct sound is much diminished compared to the former case. In the case of semi-underground structure without absorption treatment shown in the series of Fig.9 (c), very complicated multiple reflections inside the structure and sound propagation through the opening are seen. In the case where the sidewalls are assumed absorptive as shown in the series of Fig.9 (d), the multiple reflections and sound propagation outside are much diminished in the same manner as in the former case. In the series of Fig.9 (d), it should be noted that multiple reflection still remains between the ceiling and the road surface.

    (a) Depressed structurewithout absorption

    (b) Depressed structurewith absorption

    5 m

    6 m

    20 m

    S

    5 m

    6 m

    20 m

    SAbsorption

    (c) Semi-underground structure

    without absorption(d) Semi-underground structure

    with absorption

    5 m20 m

    S7.5 m

    5 m6

    m20 m

    Absorption7.5 m

    S

    Figure 8 Variation of depressed or semi-underground road structure under investigation

    50 ms

    100 ms

    150 ms

    50 ms

    100 ms

    150 ms

    50 ms

    100 ms

    150 ms

    50 ms

    100 ms

    150 ms

    S S S S

    (a) (b) (c) (d)

    Figure 9 Sound reflection and diffraction around depressed or semi-underground road structure.

  • Sound propagation over undulations of ground When assessing environmental noise, sound propagation on uneven ground with gentle undulations often becomes problem. Especially in assessment of noise radiated from construction work, the difficulty of the noise prediction is serious and calculation model for such geography is being discussed in Japan. In this section, sound propagation over the undulations of ground is introduced. In this study, five types of ground (Type 0: flat surface, Type 1 and 2 simple convex and concave surfaces, Type 3 and 4: two cases of combination of convex and concave surfaces) which extend over 800 m were set. Radius of curvature was made 1,000 m for types 1, 2, 3 and 4. In this calculation, spatial grid size became relatively large and therefore sound pressure response has mainly low frequency components. As an example of the calculation result, snap shot of transient sound pressure distribution of pulse propagation is shown in Fig. 10.

    SS

    SS

    SS

    SS

    SS

    400m400m

    (Height = 1.5 m)

    Radius of curvature: 1,000 m

    Radius of curvature: 1,000 m

    Type 0

    Type 1

    Type 2

    Type 3

    Type 4

    Figure 10 Instantaneous sound pressure distribution at 1.0 s after a impulsive source is generated

  • When the ground has a concave profile as Type 1, amplitude of propagating sound near the ground is emphasized. On the contrary, the amplitude of sound decreases when the ground has convex profile as Type 2. This tendency is clearly seen in Fig. 10 by the change of the shade of the wave fronts. In the case where the ground has successive smooth unevenness as Type 3 and 4, it is seen that the amplitude of sound changes by position of the sound source; in Type 4 where the source is located on a bottom of concave, amplitude of sound is weak near the ground, whereas in the Type 3 where it is on the top of the convex, sound wave has large amplitude.

    CONCLUSIONS

    In this report, some examples of sound field visualization based on the numerical calculation using the FDTD method have been presented. These results can be demonstrated effectively by computer-animation. Visualization technique may contribute to intuitive understanding of acoustic phenomena –reflection, diffraction and interference- in arbitrary sound fields and therefore it will be very useful not only for acoustic education but also for practical acoustic engineering. It should be added that the detailed quantitative evaluation is also possible by squaring and integrating the impulse responses obtained by the FDTD method in each frequency band. Hence, the FDTD method is effectively utilized for engineering purposes.

    REFERENCES

    [1] Takatoshi Yokota, Shinichi Sakamoto, Hideki Tachibana, ”Sound field simulation method by combining finite difference time domain calcuration and multi-channel reproduction technique,” Acoust. Sci. & Tech., 25, (1) 5-23 (2004) [2] Takatoshi Yokota, Shinichi Sakamoto, Hideki Tachibana, “Visualization of sound propagation and scattering in rooms,” Acoust. Sci. & Tech., 23, (1) 40-46 (2002) [3] Shinichi Sakamoto, Takuma Seimiya, Hideki Tachibana, “Visualization of sound reflection and diffraction using finite difference time domain method,” Acoust. Sci. & Tech., 23, (1) 34-39 (2002) [4] J. P. Berenger, “A perfectly matched layer for the absorpton of electro magnetic waves,” J. Comput. Phys., 114 (1) 185-200 (1994) [5] Shinichi Sakamoto, Takuma Seimiya, Hideki Tachibana, “Study on sound attenuation performance of noise barrier with various sectional shapes,” Proceedings of the 2000 meeting of the Institute of Noise Control Engineering of Japan, 141-144 (2000.9) [6] Shinichi Sakamoto, Hideki Tachibana, “FDTD analysis of diffraction over various types of noise barriers,” Proceedings of ICA 2004, I, 525-526 (2004.4) [7] Shinichi Sakamoto, Hedeki Tachibana, “Numerical analysis on noise attenuation performance of embankment,” Proceedings of inter-noise2003, in CD-ROM paper No. N918 (2003.8) [8] Shinichi Sakamoto, Hedeki Tachibana, “Study on simplified calculation model for prediction of noise radiation from semi-underground roads,” Proceedings of inter-noise 2002, in CD-ROM paper No. N634 (2002.8)

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