PDF

Small Concert Hall Acoustics
Introduction
Designing structures and open spaces with respect to sound quality is important for concert halls, outdoor environments, and even the rooms of a house. Simulating acoustics in the high-frequency limit, where the wavelength is smaller than the geometrical features, is best done with ray acoustics.
This tutorial model shows the basic steps and principles used when setting up a model using the Ray Acoustics physics interface. In the model, the acoustics of a small concert hall is analyzed. The model setup includes an omnidirectional sound source, wall boundary conditions for specular and diffuse scattering, surface sound pressure level evaluation, analyzing the impulse response, evaluation of objective room acoustic metrics, and a reflectogram. The metric results are compared to simple analytical estimates.
Model Definition
In this model the acoustics of a generic “small concert hall” are analyzed. The model is that of a listening environment with a volume of 460 m3 and a total surface area of 390 m2. The listening environment is fitted with absorbers and diffusers; their location is not particularly optimized and does probably not follow design rules. The aim of this tutorial is to describe the important modeling steps to perform a room acoustics simulation using ray tracing. The geometry of the concert hall is depicted in Figure 1.
Figure 1: Geometry of the small concert hall.
An omnidirectional source is located at the coordinates (xs, ys, zs) near the stage. It generates a pulse that has an SPL of 100 dB at 1 m from the source. The receiver (microphone) is located at the coordinates (xr, yr, zr). These are parameters found under Global Definitions > Parameters 1. The location of the receiver can be changed in postprocessing, while the location of the source needs to be changed before running the model.
The absorption properties of the various surfaces (windows, seats, diffusers, floor, entrance, walls, and absorbers) are generic values taken from Ref. 1 and 2. The data is given in octave band values and imported from the file small_concert_hall_absorption_parameters.txt file into an interpolation function (lookup table). Moreover, the (intensity) attenuation of air is imported from the file small_concert_hall_volume_absorption.txt. Note that when the attenuation coefficient m (loaded from the file) is entered in the Material Properties of Exterior and Unmeshed Domains section, it is the amplitude attenuation αext = 0.5·m that should be used.
Figure 2: Ray location and SPL after 10 ms.
Results and Discussion
The local wavefront sound pressure level (SPL) is depicted in Figure 2 after 10 ms and in Figure 3 after 20 ms propagation for the 16 kHz frequency band. At this frequency the volume attention is the largest. When the compute intensity option is selected in the Ray Acoustics interface, wavefront curvature, intensity, and SPL is calculated along each ray. They allow visualization of the (spatially) local acoustic properties. However, it is the acoustic power transported by each ray that is important when calculating the impulse response (IR) and when visualizing the sound pressure level at surfaces. This means that the compute power option should always be selected for IR computation, while the compute intensity can be turned off. Only selecting Compute power will also make the model run slightly faster and reduce the number of degrees of freedom (DOFs) solved for. The Count reflections option is also necessary when analyzing the IR.
Figure 3: Ray location and field SPL after 20 ms.
The temporal impulse response (IR) for the default source location configuration used in the model is depicted in Figure 4. The frequency domain (FFT) of the IR is depicted in Figure 5. No smoothing nor windowing is used in the plot. The IR is further analyzed using the Energy Decay subfeature to the Impulse Response plot. The feature allows the computation of the objective room acoustic metrics like clarity C, definition D, early decay time EDT, center time ts, reverberation times T20, T30, T60, and the STI. The level decay curves for the 6 octave bands used in the model (computed by the Energy Decay subfeature) are depicted in Figure 6. The metrics can be found in the Objective Quality Metrics table in the model (Results > Tabels). The values are depicted graphically in Figure 9 and Figure 10.
When an IR is reconstructed from a ray tracing simulation, information is inferred and put back into the time signal using the temporal filter kernels. The quality of the simulated IR increases with the number of rays (this model uses 20,000) as well as the frequency resolution of the absorption, scattering, and source data (this data can be difficult to get from vendors but can often be simulated). In this model, octave band resolution is used. The Impulse Response plot also allows the use of 1/3 octave and 1/6 octave frequency resolution.
Figure 4: Temporal impulse response computed at the receiver location.
Figure 5: FFT of the impulse response (no smoothing/windowing is used).
Figure 6: Level decay curves for the 6 octave bands used in the model.
The sound pressure level in a cross section located above the seating section is depicted in Figure 7 for the 16 kHz band. It is calculated using the Sound Pressure Level Calculation feature, available as a subnode to all Wall boundary conditions. In this case it is added to a transparent surface (Pass through used as Wall condition). The feature can be added to all other walls to postprocess the SPL distribution there if necessary.
Figure 7: SPL in a cross section 60 cm above the ground at the location of the audience.
In the ray tracing method, the intensity I and RMS pressure prms of the nth ray detected by the receiver sphere is expressed as
where Vr is the receiver volume, Lr is the distance traveled by the ray inside the receiver, and Qn is the power carried by the ray (see, for example, Ref. 3). The intensity is evaluated using the expression re1dist*rac.Q/re1vol. Plotting this information in a Ray plot as function of the arrival time yields the (discrete time) energy impulse response or reflectogram. It is plotted for the 500 Hz and the 16 kHz octave bands in Figure 8. The slope of the curves (point data) gives a visual indication of the reverberation time of the room. In Figure 8 approximate trend lines have been added manually; their slope (60 dB down which is 6 decades for log10(In)) gives an estimate of the T60 reverberation time. In this case about 0.5 s for the 16 kHz band and 1 s for the 500 Hz band. These values are seen to fit well with the computed values below.
Figure 8: The raw data of the energetic impulse response or reflectogram. The slope represents the reverberation time in the given octave band.
A comparison between the computed value of T60 and simple statistical estimates is shown in Figure 9. To plot the data from the results table the Table Graph plot is used. The estimated values are calculated using the Sabine and Eyring equations used in statistical room acoustics
where V is the room volume, S is the total surface area, m is the volume attenuation, and is the average wall absorption (see Ref. 2). The results show quantitative agreement. It is not expected that the Sabine and Eyring predictions match the more detailed ray tracing results exactly.
Selected room acoustic metrics are plotted as function of the octave band center frequency in Figure 10. The definition, the clarity, and the center time metrics are also compared to analytical estimates in the figures. The estimates are based on analytical models of the direct energy, early energy, and late energy (see Ref. 1). They are defined in the Definitions > Variables: Quality Metric Estimates.
Definition (D or D50) gives a metric for syllable intelligibility. In this room it is above 50% for all bands which is acceptable. The clarity metric C80 is used to characterize the transparency of music, for concert halls typical values lie between -5 to +3 dB. In this case the design is not optimal for the higher octave bands. The center time is another metric that correlates to speech intelligibility. All metrics should be estimated taking their just noticeable difference (JND) into account.
Figure 9: Reverberation time estimates based on the Sabine and Eyring formula compared to the computed reverberation time.
The speech transmission index STI is a single valued metric for speech intelligibility. It is based on modulation transfer function values (14 frequencies) and 7 octave bands. The Modulation transfer function can be plotted using the Energy Decay subfeature. The STI is computed as a single value that combines the information in the 7 bands. To get the single metric, change the Band type to Broadband. Making these changes this gives a STI value of 0.63 (this indicates good intelligibility). Note that the standard does specify using also the 125 and 250 Hz octave bands (they are not included in this model). The STI values plotted as function of octave band center frequency in Figure 10 are computed based on the apparent signal to noise ratio in each band. When Broadband is selected the values in each band contribute with the appropriate weighting.
Figure 10: Objective room acoustic metrics clarity, definition, reverberation times, and STI plotted as function of octave band center frequency. The clarity and definition metrics are compared to analytical estimates. The center time (not shown here) can be seen in the plots in the model.
Notes About the COMSOL Implementation
There are several options that can be selected on the Results node that are useful when working with ray acoustic models and especially when evaluating the impulse response.
When first setting up plots, it is useful to select the Only plot when requested option as some plots take a long time to render. Another trick is to use only a few rays initially.
Once the plots are set up, then before running the model (with a large number of rays), select the Recompute all plot data after solving option. Once the model has solved the plots will be rendered. This is very useful when running the model over lunch break or over night since rendering the IR plot often takes longer time than solving the model.
Before saving the model, remember to set the Save plot data list to On. Then all plots do not need to be re-rendered once the model is opened again.
References
1. M. Vorländer, Auralization, Fundamentals of Acoustics, Modeling, Simulation, Algorithms and Acoustic Virtual Reality, Springer, 2008.
2. H. Kuttruff, Room Acoustics, CRC Press, 2009.
3. Z. Xiangyang, C. Ke'an, and S. Jincai, “On the accuracy of the ray-tracing algorithms based on various sound receiver models,” Appl. Acoust., vol. 64, pp. 433–441, 2003.
Application Library path: Acoustics_Module/Building_and_Room_Acoustics/small_concert_hall
Modeling Instructions
This section contains the modeling instructions for the Absorptive Muffler model. They are followed by the Geometry Sequence Instructions section.
From the File menu, choose New.
New
In the New window, click  Model Wizard.
Model Wizard
1
In the Model Wizard window, click  3D.
2
In the Select Physics tree, select Acoustics>Geometrical Acoustics>Ray Acoustics (rac).
3
Click Add.
4
Click  Study.
5
In the Select Study tree, select Preset Studies for Selected Physics Interfaces>Ray Tracing.
6
Geometry 1
The geometry is set up by importing a geometry sequence. The sequence imports the small concert hall geometry and sets up several selections. The predefined selections simplify the rest of the model setup.
1
In the Geometry toolbar, click  Insert Sequence.
2
3
In the Geometry toolbar, click  Build All.
4
Click the  Zoom Extents button in the Graphics toolbar.
Import the model parameters form a file. The parameters include the band center frequency f0, the location of the source and receiver, as well as the room volume.
Global Definitions
Parameters 1
1
In the Model Builder window, under Global Definitions click Parameters 1.
2
In the Settings window for Parameters, locate the Parameters section.
3
Click  Load from File.
4
Proceed and set up interpolation functions for the absorption coefficients of the different surfaces in the concert hall. The data is easily stored in one .txt file. Also define an interpolation function for the intensity attenuation of air (given at 50 % relative humidity and 20 deg. C).
Interpolation 1 (int1)
1
In the Home toolbar, click  Functions and choose Global>Interpolation.
2
In the Settings window for Interpolation, locate the Definition section.
3
From the Data source list, choose File.
4
Click Browse.
5
6
In the Number of arguments text field, type 1.
7
Click Import.
8
Find the Functions subsection. In the table, enter the following settings:
9
Locate the Interpolation and Extrapolation section. From the Interpolation list, choose Nearest neighbor.
10
Locate the Units section. In the Arguments text field, type Hz.
11
In the Function text field, type 1.
Interpolation 2 (int2)
1
In the Home toolbar, click  Functions and choose Global>Interpolation.
2
In the Settings window for Interpolation, locate the Definition section.
3
From the Data source list, choose File.
4
Click Browse.
5
6
Click Import.
7
In the Function name text field, type m_air.
8
Locate the Interpolation and Extrapolation section. From the Interpolation list, choose Nearest neighbor.
9
Locate the Units section. In the Arguments text field, type Hz.
10
In the Function text field, type 1/m.
Now import the variables that define the room acoustic quality metric estimates. They include the reverberation time (T60), based on the Sabine and Eyring estimation equations, clarity, definition, and center time. This also requires setting up integration operators for all the surfaces.
Definitions
Variables: Quality Metric Estimates
1
In the Model Builder window, expand the Component 1 (comp1)>Definitions node.
2
Right-click Definitions and choose Variables.
3
In the Settings window for Variables, type Variables: Quality Metric Estimates in the Label text field.
4
Locate the Variables section. Click  Load from File.
5
Integration 1 (intop1)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, type intop_windows in the Operator name text field.
3
Locate the Source Selection section. From the Geometric entity level list, choose Boundary.
4
From the Selection list, choose Windows.
Integration 2 (intop2)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, type intop_seats in the Operator name text field.
3
Locate the Source Selection section. From the Geometric entity level list, choose Boundary.
4
From the Selection list, choose Seats.
Integration 3 (intop3)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, type intop_diffusers in the Operator name text field.
3
Locate the Source Selection section. From the Geometric entity level list, choose Boundary.
4
From the Selection list, choose Diffusers.
Integration 4 (intop4)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, type intop_floor in the Operator name text field.
3
Locate the Source Selection section. From the Geometric entity level list, choose Boundary.
4
From the Selection list, choose Floor.
Integration 5 (intop5)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, type intop_entrance in the Operator name text field.
3
Locate the Source Selection section. From the Geometric entity level list, choose Boundary.
4
From the Selection list, choose Entrance.
Integration 6 (intop6)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, type intop_walls in the Operator name text field.
3
Locate the Source Selection section. From the Geometric entity level list, choose Boundary.
4
From the Selection list, choose Walls.
Integration 7 (intop7)
1
In the Definitions toolbar, click  Nonlocal Couplings and choose Integration.
2
In the Settings window for Integration, type intop_absorbers in the Operator name text field.
3
Locate the Source Selection section. From the Geometric entity level list, choose Boundary.
4
From the Selection list, choose Absorbers.
Proceed to set up and define the physics and boundary conditions of the model. To compute the impulse response, it is necessary to model the power along the rays and count the reflections. In the model the intensity is also computed along the rays. The intensity represents spatially local properties of the acoustic field approximated by the rays. The model only uses a surface mesh. Propagation in the unmeshed domains requires the definition of material properties at the interface level (in the section Material Properties of Exterior and Unmeshed Domains). Set up boundary conditions for the different walls (boundaries).
Ray Acoustics (rac)
1
In the Model Builder window, under Component 1 (comp1) click Ray Acoustics (rac).
2
In the Settings window for Ray Acoustics, locate the Intensity Computation section.
3
From the Intensity computation list, choose Compute intensity and power.
4
Locate the Material Properties of Exterior and Unmeshed Domains section. In the cext text field, type c0.
5
In the ρext text field, type rho0.
6
In the αext text field, type 0.5*m_air(f0).
Multiplication by 0.5 is necessary as the input in COMSOL is defined for the amplitude attenuation and not the intensity attenuation (as given in the interpolation data).
7
Locate the Additional Variables section. Select the Count reflections check box.
Ray Properties 1
1
In the Model Builder window, under Component 1 (comp1)>Ray Acoustics (rac) click Ray Properties 1.
2
In the Settings window for Ray Properties, locate the Ray Properties section.
3
In the f text field, type f0.
Wall: Walls
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: Walls in the Label text field.
3
Locate the Boundary Selection section. From the Selection list, choose Walls.
4
Locate the Wall Condition section. From the Wall condition list, choose Specular reflection.
5
Locate the Reflection Coefficient Model section. In the α text field, type a_walls(f0).
Wall: Entrance
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: Entrance in the Label text field.
3
Locate the Boundary Selection section. From the Selection list, choose Entrance.
4
Locate the Wall Condition section. From the Wall condition list, choose Specular reflection.
5
Locate the Reflection Coefficient Model section. In the α text field, type a_entrance(f0).
Wall: Windows
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: Windows in the Label text field.
3
Locate the Boundary Selection section. From the Selection list, choose Windows.
4
Locate the Wall Condition section. From the Wall condition list, choose Specular reflection.
5
Locate the Reflection Coefficient Model section. In the α text field, type a_windows(f0).
Wall: Floor
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: Floor in the Label text field.
3
Locate the Boundary Selection section. From the Selection list, choose Floor.
4
Locate the Wall Condition section. From the Wall condition list, choose Specular reflection.
5
Locate the Reflection Coefficient Model section. In the α text field, type a_floor(f0).
Wall: Diffusers
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: Diffusers in the Label text field.
3
Locate the Boundary Selection section. From the Selection list, choose Diffusers.
4
Locate the Wall Condition section. From the Wall condition list, choose Mixed diffuse and specular reflection.
5
In the γs text field, type 1-s_diffuser.
6
Locate the Reflection Coefficients Model section. In the αs text field, type a_diffuser(f0).
7
In the αd text field, type a_diffuser(f0).
In this model the scattering coefficient s_diffuser is constant across the frequency bands. It can of course also be defined as an interpolation function that depends on f0.
Wall: Seats
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: Seats in the Label text field.
3
Locate the Boundary Selection section. From the Selection list, choose Seats.
4
Locate the Wall Condition section. From the Wall condition list, choose Specular reflection.
5
Locate the Reflection Coefficient Model section. In the α text field, type a_seats(f0).
Wall: Absorbers
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: Absorbers in the Label text field.
3
Locate the Boundary Selection section. From the Selection list, choose Absorbers.
4
Locate the Wall Condition section. From the Wall condition list, choose Specular reflection.
5
Locate the Reflection Coefficient Model section. In the α text field, type a_absorbers(f0).
Wall: SPL cross section
1
In the Physics toolbar, click  Boundaries and choose Wall.
2
In the Settings window for Wall, type Wall: SPL cross section in the Label text field.
3
Locate the Wall Condition section. From the Wall condition list, choose Pass through.
The Pass through option is used here as this surface only is meant for visualizing the SPL in a cross section. Use Wireframe rendering to select the surface that is located inside the concert hall.
4
Click the  Wireframe Rendering button in the Graphics toolbar.
5
Sound Pressure Level Calculation 1
1
In the Physics toolbar, click  Attributes and choose Sound Pressure Level Calculation.
2
In the Settings window for Sound Pressure Level Calculation, locate the Smoothing section.
3
Select the Compute smoothed accumulated variable check box.
Release from Grid 1
1
In the Physics toolbar, click  Global and choose Release from Grid.
2
In the Settings window for Release from Grid, locate the Initial Coordinates section.
3
In the qx,0 text field, type x_s.
4
In the qy,0 text field, type y_s.
5
In the qz,0 text field, type z_s.
6
Locate the Ray Direction Vector section. From the Ray direction vector list, choose Spherical.
7
In the Nw text field, type Nrays.
8
Locate the Total Source Power section. In the Psrc text field, type P0.
Ray Termination 1
1
In the Physics toolbar, click  Global and choose Ray Termination.
2
In the Settings window for Ray Termination, locate the Termination Criteria section.
3
From the Spatial extents of ray propagation list, choose Bounding box, from geometry.
4
From the Additional termination criteria list, choose Intensity.
5
In the Ith text field, type 1e-14[W/m^2].
Mesh 1
Free Triangular 1
1
In the Mesh toolbar, click  Boundary and choose Free Triangular.
2
In the Settings window for Free Triangular, locate the Boundary Selection section.
3
From the Selection list, choose All boundaries.
Size
1
In the Model Builder window, click Size.
2
In the Settings window for Size, locate the Element Size section.
3
From the Predefined list, choose Finer.
Size 1
1
In the Model Builder window, right-click Free Triangular 1 and choose Size.
Add a finer mesh on the surface where the SPL is computed.
2
In the Settings window for Size, locate the Geometric Entity Selection section.
3
Click  Clear Selection.
4
5
Locate the Element Size section. Click the Custom button.
6
Locate the Element Size Parameters section. Select the Maximum element size check box.
7
8
Click  Build All.
Proceed and solve the model by adding a parametric sweep over the center frequency variable f0. This represents the center frequency of the octave bands analyzed in this model, in order to get a broadband response. The first time you set up and solve the model it can be useful to reduce the number of rays by changing the value of the parameter Nrays to, for example, 1000. This will make solving and postprocessing faster. Remember that the quality of the results in acoustic ray tracing increase for an increasing number of rays and more narrow frequency bands (you need to have wall absorption data with the desired resolution). In the Ray Acoustics interface the impulse response plot can handle octave, 1/3 octave, and 1/6 octave data.
Study 1
Step 1: Ray Tracing
1
In the Model Builder window, under Study 1 click Step 1: Ray Tracing.
2
In the Settings window for Ray Tracing, locate the Study Settings section.
3
From the Time unit list, choose s.
4
In the Output times text field, type 0 1.6.
For optimal performance only enter 0 and the end time for the simulation. In postprocessing, when reconstructing the impulse response, additional exact time steps for all the wall reflections are used and rendered.
Parametric Sweep
1
In the Study toolbar, click  Parametric Sweep.
Using the parametric sweep is important as this gives the frequency resolution (here in full octaves). The ray propagation model is solved once per frequency band. The data is collected in postprocessing, by the receiver dataset and the impulse response plot, to generate the broadband impulse response.
2
In the Settings window for Parametric Sweep, locate the Study Settings section.
3
4
Click  Range.
5
In the Range dialog box, choose ISO preferred frequencies from the Entry method list.
6
In the Start frequency text field, type 500.
7
In the Stop frequency text field, type 20000.
8
Click Replace.
Solving the model takes a couple of minutes and uses less than 2 GB of RAM (depending on your hardware). This will increase for an increasing number of rays.
9
In the Study toolbar, click  Compute.
Results
Ray Trajectories (rac)
1
In the Settings window for 3D Plot Group, locate the Data section.
2
From the Time (s) list, choose Interpolation.
3
In the Time text field, type 10[ms].
4
In the Ray Trajectories (rac) toolbar, click  Plot.
Ray Trajectories 1
1
In the Model Builder window, expand the Ray Trajectories (rac) node, then click Ray Trajectories 1.
2
In the Settings window for Ray Trajectories, locate the Coloring and Style section.
3
Find the Line style subsection. From the Type list, choose None.
4
Find the Point style subsection. From the Type list, choose Point.
Color Expression 1
1
In the Model Builder window, expand the Ray Trajectories 1 node, then click Color Expression 1.
2
In the Settings window for Color Expression, locate the Expression section.
3
In the Expression text field, type rac.Lp.
4
In the Ray Trajectories (rac) toolbar, click  Plot.
This should reproduce the image in Figure 2.
Ray Trajectories (rac)
1
In the Model Builder window, click Ray Trajectories (rac).
2
In the Settings window for 3D Plot Group, locate the Data section.
3
In the Time text field, type 20[ms].
4
In the Ray Trajectories (rac) toolbar, click  Plot.
This should reproduce the image in Figure 3.
On the Results node you have several options that are useful when postprocessing ray tracing simulations, where rendering plots can be time consuming. This is especially true for the impulse response plots. While setting up plots, it is useful to select Only plot when requested such that the plots are not generated every time you change an option. It is also good practice to save the plots in the model such that they are already rendered when you open your model at a later stage. Finally, once you have set up all the plots and you are ready to run the model again, it can be useful to enable Recompute all plot data after solving. All plots will then be recomputed after the model is solved, for example, running over lunch.
5
In the Model Builder window, click Results.
6
In the Settings window for Results, locate the Update of Results section.
7
Select the Only plot when requested check box.
8
Locate the Save Data in the Model section. From the Save plot data list, choose On.
Now set up the Receiver dataset used for creating the impulse response and subsequent analysis.
Receiver 3D - All Bands
1
In the Model Builder window, expand the Results>Datasets node.
2
Right-click Datasets and choose More 3D Datasets>Receiver 3D.
3
In the Settings window for Receiver 3D, type Receiver 3D - All Bands in the Label text field.
4
Locate the Receiver section. Find the Center subsection. In the x text field, type x_r.
5
In the y text field, type y_r.
6
In the z text field, type z_r.
7
Find the Radius subsection. In the Number of rays text field, type Nrays.
8
In the Room volume text field, type Vol.
9
In the Source-receiver distance text field, type dsr.
The default Expression option for the receiver radius is good for classical room acoustics applications (like in this example). If ray tracing is used in smaller spaces, like a car cabin, it is recommended to switch to a user defined radius.
Receiver 3D - 500 Hz Band
1
In the Model Builder window, right-click Receiver 3D - All Bands and choose Duplicate.
2
In the Settings window for Receiver 3D, type Receiver 3D - 500 Hz Band in the Label text field.
3
Locate the Data section. From the Parameter selection (f0) list, choose From list.
4
In the Parameter values (f0 (Hz)) list, select 500.
Receiver 3D - 16 kHz Band
1
In the Model Builder window, right-click Receiver 3D - 500 Hz Band and choose Duplicate.
2
In the Settings window for Receiver 3D, type Receiver 3D - 16 kHz Band in the Label text field.
3
Locate the Data section. From the Parameter selection (f0) list, choose From list.
4
In the Parameter values (f0 (Hz)) list, select 16000.
Impulse Response
1
In the Results toolbar, click  1D Plot Group.
2
In the Settings window for 1D Plot Group, type Impulse Response in the Label text field.
3
Locate the Data section. From the Dataset list, choose Receiver 3D - All Bands.
Impulse Response 1
1
In the Impulse Response toolbar, click  More Plots and choose Impulse Response.
To get sharper filters you can modify some settings in the Advanced section.
2
In the Settings window for Impulse Response, click to expand the Advanced section.
3
In the Np text field, type 22050.
4
In the δ text field, type 0.001.
Rendering the impulse response will typically take one or two minutes (depending on hardware, number of rays, and frequency band resolution). Once the plot has been generated (the first time) the necessary ray data is cached and any subsequent changes/updates of the plot is faster.
5
In the Impulse Response toolbar, click  Plot.
This should reproduce the impulse response shown in Figure 4. The impulse response is the most important result of this model. The signal can be exported under the Export node and used for further analysis in an external signal processing tool. The response is reconstructed from the ray data detected by the Receiver dataset (arrival time, power, and band center frequency). It has a default sampling frequency of 44100 Hz. This can also be changed under the Advanced section in the plot settings window.
Plot 1
1
Right-click Impulse Response 1 and choose Add Plot Data to Export.
2
In the Settings window for Plot, locate the Output section.
3
From the File type list, choose WAVE audio file (*.wav).
4
In the Filename text field, type small_concert_hall_impulse_response.wav.
5
Click to expand the Advanced section. From the Quantization level list, choose 16-bit.
Click Export to produce a wav file with the impulse response. This file could be used for auralization or analysis with other tools. Remember to disable any Energy Decay subfeature before exporting.
Proceed to analyze the impulse response with the Energy Decay subfeature. This will create a plot of the level/energy decay and a table with the objective quality metrics.
Energy Decay 1
1
In the Model Builder window, expand the Results>Impulse Response node.
2
Right-click Impulse Response 1 and choose Energy Decay.
3
In the Settings window for Energy Decay, locate the Display section.
4
From the Band type list, choose Individual bands.
5
From the Band frequency list, choose All.
6
From the Plot list, choose Level decay.
7
Right-click Energy Decay 1 and choose Show Legends.
8
In the Impulse Response toolbar, click  Plot.
To show the impulse response signal again, simply disable the Energy Decay subfeature and click Plot again.
For the sake of this tutorial, the impulse response is generated again and an FFT of the transient signal is performed (duplicate the plot and disable the Energy Decay subfeature). Since a new plot is now generated, the IR data has to be computed again. Creating the plot based on the existing IR plot would have been faster as the data is cached.
Impulse Response 1
1
In the Model Builder window, right-click Impulse Response and choose Duplicate.
2
Expand the Impulse Response 1 node.
Energy Decay 1
1
In the Model Builder window, expand the Impulse Response 1 node.
2
Right-click Energy Decay 1 and choose Disable.
Impulse Response FFT
1
In the Model Builder window, under Results click Impulse Response 1.
2
In the Settings window for 1D Plot Group, type Impulse Response FFT in the Label text field.
3
Locate the Axis section. Select the x-axis log scale check box.
4
Select the y-axis log scale check box.
Impulse Response 1
1
In the Model Builder window, expand the Impulse Response FFT node, then click Impulse Response 1.
2
In the Settings window for Impulse Response, locate the x-Axis Data section.
3
From the Transformation list, choose Frequency spectrum.
4
Select the Frequency range check box.
5
In the Minimum text field, type 100.
6
In the Maximum text field, type 20000.
7
In the Impulse Response FFT toolbar, click  Plot.
This should reproduce the image in Figure 5.
8
In the Model Builder window, click Results.
9
In the Settings window for Results, locate the Update of Results section.
10
Clear the Only plot when requested check box.
Cross Section SPL
1
In the Home toolbar, click  Add Plot Group and choose 3D Plot Group.
2
In the Settings window for 3D Plot Group, type Cross Section SPL in the Label text field.
3
Locate the Data section. From the Dataset list, choose Study 1/Parametric Solutions 1 (sol2).
Surface 1
1
Right-click Cross Section SPL and choose Surface.
2
In the Settings window for Surface, click Replace Expression in the upper-right corner of the Expression section. From the menu, choose Component 1 (comp1)>Ray Acoustics>Accumulated variables>Wall intensity comp1.rac.wall9.spl1.Iw>rac.wall9.spl1.Lp - Sound pressure level - dB.
3
In the Cross Section SPL toolbar, click  Plot.
This should reproduce the image in Figure 7. The 16 kHz band is chosen per default. A smoothed variable for the SPL also exists rac.wall9.spl1.Lp_sm.
Reflectogram
1
In the Home toolbar, click  Add Plot Group and choose 1D Plot Group.
2
In the Settings window for 1D Plot Group, type Reflectogram in the Label text field.
3
Click to expand the Title section. From the Title type list, choose Label.
4
Locate the Plot Settings section. Select the x-axis label check box.
5
6
Select the y-axis label check box.
7
8
Locate the Data section. From the Dataset list, choose None.
9
Locate the Axis section. Select the y-axis log scale check box.
Ray 1
1
In the Reflectogram toolbar, click  More Plots and choose Ray.
2
In the Settings window for Ray, locate the Data section.
3
From the Dataset list, choose Receiver 3D - 500 Hz Band.
4
Locate the y-Axis Data section. In the Expression text field, type re1dist*rac.Q/re1vol.
5
Click to expand the Coloring and Style section. Find the Line style subsection. From the Line list, choose None.
6
Find the Line markers subsection. From the Marker list, choose Point.
7
From the Positioning list, choose In data points.
8
Click to expand the Legends section. From the Legends list, choose Manual.
9
Select the Show legends check box.
10
Ray 2
1
Right-click Ray 1 and choose Duplicate.
2
In the Settings window for Ray, locate the Data section.
3
From the Dataset list, choose Receiver 3D - 16 kHz Band.
4
Locate the Legends section. In the table, enter the following settings:
5
In the Reflectogram toolbar, click  Plot.
This should reproduce the image in Figure 8.
T60 - Estimates and Model
1
In the Home toolbar, click  Add Plot Group and choose 1D Plot Group.
2
In the Settings window for 1D Plot Group, type T60 - Estimates and Model in the Label text field.
3
Locate the Data section. From the Dataset list, choose Study 1/Parametric Solutions 1 (sol2).
4
From the Time selection list, choose First.
5
Click to expand the Title section. From the Title type list, choose Label.
6
Locate the Axis section. Select the x-axis log scale check box.
7
Locate the Legend section. From the Position list, choose Lower left.
Global 1
1
Right-click T60 - Estimates and Model and choose Global.
2
In the Settings window for Global, locate the y-Axis Data section.
3
4
Locate the x-Axis Data section. From the Axis source data list, choose f0.
5
Click to expand the Coloring and Style section. Find the Line markers subsection. From the Marker list, choose Star.
6
From the Positioning list, choose In data points.
Table Graph 1
1
In the Model Builder window, right-click T60 - Estimates and Model and choose Table Graph.
2
In the Settings window for Table Graph, locate the Data section.
3
From the x-axis data list, choose fc (Hz).
4
From the Plot columns list, choose Manual.
5
In the Columns list, select T60 (s).
6
Locate the Coloring and Style section. Find the Line markers subsection. From the Marker list, choose Circle.
7
From the Positioning list, choose In data points.
8
Click to expand the Legends section. Select the Show legends check box.
9
In the Suffix text field, type - Ray acoustics.
10
In the T60 - Estimates and Model toolbar, click  Plot.
This should reproduce the image in Figure 9.
Definition
1
In the Home toolbar, click  Add Plot Group and choose 1D Plot Group.
2
In the Settings window for 1D Plot Group, type Definition in the Label text field.
3
Locate the Data section. From the Dataset list, choose Study 1/Parametric Solutions 1 (sol2).
4
From the Time selection list, choose First.
5
Click to expand the Title section. From the Title type list, choose Label.
6
Locate the Axis section. Select the x-axis log scale check box.
7
Locate the Legend section. From the Position list, choose Upper left.
Global 1
1
Right-click Definition and choose Global.
2
In the Settings window for Global, locate the y-Axis Data section.
3
4
Locate the x-Axis Data section. From the Axis source data list, choose f0.
5
Click to expand the Coloring and Style section. Find the Line markers subsection. From the Marker list, choose Star.
6
From the Positioning list, choose In data points.
Table Graph 1
1
In the Model Builder window, right-click Definition and choose Table Graph.
2
In the Settings window for Table Graph, locate the Data section.
3
From the x-axis data list, choose fc (Hz).
4
From the Plot columns list, choose Manual.
5
In the Columns list, select D (%).
6
Locate the Coloring and Style section. Find the Line markers subsection. From the Marker list, choose Circle.
7
From the Positioning list, choose In data points.
8
Click to expand the Legends section. Select the Show legends check box.
9
In the Suffix text field, type - Ray acoustics.
10
In the Definition toolbar, click  Plot.
Clarity
1
Right-click Definition and choose Duplicate.
2
In the Settings window for 1D Plot Group, type Clarity in the Label text field.
Global 1
1
In the Model Builder window, expand the Clarity node, then click Global 1.
2
In the Settings window for Global, locate the y-Axis Data section.
3
Table Graph 1
1
In the Model Builder window, click Table Graph 1.
2
In the Settings window for Table Graph, locate the Data section.
3
In the Columns list, choose C50 (dB) and C80 (dB).
4
In the Clarity toolbar, click  Plot.
Center Time
1
In the Model Builder window, right-click Clarity and choose Duplicate.
2
In the Settings window for 1D Plot Group, type Center Time in the Label text field.
3
Locate the Legend section. From the Position list, choose Lower left.
Global 1
1
In the Model Builder window, expand the Center Time node, then click Global 1.
2
In the Settings window for Global, locate the y-Axis Data section.
3
Table Graph 1
1
In the Model Builder window, click Table Graph 1.
2
In the Settings window for Table Graph, locate the Data section.
3
In the Columns list, select ts (s).
4
In the Center Time toolbar, click  Plot.
Reverberation Times
1
In the Model Builder window, right-click Center Time and choose Duplicate.
2
In the Settings window for 1D Plot Group, type Reverberation Times in the Label text field.
3
Locate the Legend section. From the Position list, choose Lower left.
Global 1
1
In the Model Builder window, expand the Reverberation Times node.
2
Right-click Global 1 and choose Delete.
Table Graph 1
1
In the Model Builder window, click Table Graph 1.
2
In the Settings window for Table Graph, locate the Data section.
3
In the Columns list, choose EDT (s), T20 (s), T30 (s), and T60 (s).
4
In the Reverberation Times toolbar, click  Plot.
STI
1
In the Model Builder window, right-click Reverberation Times and choose Duplicate.
2
In the Settings window for 1D Plot Group, type STI in the Label text field.
3
Locate the Legend section. From the Position list, choose Upper left.
Table Graph 1
1
In the Model Builder window, expand the STI node, then click Table Graph 1.
2
In the Settings window for Table Graph, locate the Data section.
3
In the Columns list, select STI (1).
4
In the STI toolbar, click  Plot.
Center Time, Clarity, Definition, Reverberation Times, STI
1
In the Model Builder window, under Results, Ctrl-click to select Definition, Clarity, Center Time, Reverberation Times, and STI.
2
Objective Quality Metric Plots
In the Settings window for Group, type Objective Quality Metric Plots in the Label text field.
Geometry Sequence Instructions
From the File menu, choose New.
New
In the New window, click  Blank Model.
Add Component
In the Home toolbar, click  Add Component and choose 3D.
Geometry 1
Import 1 (imp1)
1
In the Home toolbar, click  Import.
2
In the Settings window for Import, locate the Import section.
3
Click Browse.
4
5
Click Import.
6
Click the  Wireframe Rendering button in the Graphics toolbar.
Windows
1
In the Geometry toolbar, click  Selections and choose Explicit Selection.
2
In the Settings window for Explicit Selection, type Windows in the Label text field.
3
Locate the Entities to Select section. From the Geometric entity level list, choose Boundary.
4
On the object imp1, select Boundaries 60–62 only.
Seats
1
In the Geometry toolbar, click  Selections and choose Explicit Selection.
2
In the Settings window for Explicit Selection, type Seats in the Label text field.
3
Locate the Entities to Select section. From the Geometric entity level list, choose Boundary.
4
On the object imp1, select Boundary 39 only.
Diffusers
1
In the Geometry toolbar, click  Selections and choose Explicit Selection.
2
In the Settings window for Explicit Selection, type Diffusers in the Label text field.
3
Locate the Entities to Select section. From the Geometric entity level list, choose Boundary.
4
On the object imp1, select Boundaries 13, 15, 29, 30, 41, 42, 49, and 50 only.
Floor
1
In the Geometry toolbar, click  Selections and choose Explicit Selection.
2
In the Settings window for Explicit Selection, type Floor in the Label text field.
3
Locate the Entities to Select section. From the Geometric entity level list, choose Boundary.
4
On the object imp1, select Boundaries 3, 8, 12, 14, 18, and 21 only.
Entrance
1
In the Geometry toolbar, click  Selections and choose Explicit Selection.
2
In the Settings window for Explicit Selection, type Entrance in the Label text field.
3
Locate the Entities to Select section. From the Geometric entity level list, choose Boundary.
4
On the object imp1, select Boundaries 16, 19, 20, 23, 31, and 32 only.
Walls
1
In the Geometry toolbar, click  Selections and choose Explicit Selection.
2
In the Settings window for Explicit Selection, type Walls in the Label text field.
3
Locate the Entities to Select section. From the Geometric entity level list, choose Boundary.
4
On the object imp1, select Boundaries 7, 9–11, 17, 22, 24–28, 34–37, 43–48, and 51–59 only.
Absorbers
1
In the Geometry toolbar, click  Selections and choose Explicit Selection.
2
In the Settings window for Explicit Selection, type Absorbers in the Label text field.
3
Locate the Entities to Select section. From the Geometric entity level list, choose Boundary.
4
On the object imp1, select Boundaries 1, 2, 4–6, 33, and 38 only.
Form Union (fin)
1
In the Model Builder window, click Form Union (fin).
2
In the Settings window for Form Union/Assembly, click  Build Selected.