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In the Select Physics tree, select Acoustics > Ultrasound > Nonlinear Pressure Acoustics, Time Explicit (nate).
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Click Add.
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Browse to the model’s Application Libraries folder and double-click the file hifu_tissue_sample_parameters.txt.
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Locate the Definition section. In the Expression text field, type sin(omega0*t)*(1 - cos(omega0*t/5))*rect1(t).
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Locate the Units section. In the table, enter the following settings:
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Locate the Plot Parameters section. In the table, enter the following settings:
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Click
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Select the Frequency range checkbox.
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Click
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Click in the Graphics window and then press Ctrl+A to select both objects.
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Click to expand the Layers section. In the table, enter the following settings:
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Select the Layers to the right checkbox.
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Clear the Layers on bottom checkbox.
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Select the Layers on top checkbox.
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Locate the Layers section. In the table, enter the following settings:
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Select the Layers to the right checkbox.
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Clear the Layers on bottom checkbox.
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Click
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On the object fin, select Boundary 3 only.
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In the Model Builder window, expand the Domain Point Probe 1 node, then click Point Probe Expression 1 (ppb1).
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In the Model Builder window, under Component 1 (comp1) > Nonlinear Pressure Acoustics, Time Explicit (nate) click Nonlinear Pressure Acoustics, Time Explicit Model 1.
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In the Settings window for Nonlinear Pressure Acoustics, Time Explicit Model, locate the Pressure Acoustics Model section.
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In the Model Builder window, under Component 1 (comp1) right-click Materials and choose Blank Material.
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Locate the Material Contents section. In the table, enter the following settings:
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Locate the Material Contents section. In the table, enter the following settings:
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Locate the Element Size Parameters section.
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Locate the Element Size Parameters section.
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Click to expand the Adaptation section. From the Adaptive mesh refinement list, choose Adaptive mesh refinement.
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Find the Mesh element control subsection. From the Adaptation method list, choose General modification.
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In the Model Builder window, expand the Study 1 > Solver Configurations > Solution 1 (sol1) > Time-Dependent Solver 1 node, then click Adaptive Mesh Refinement.
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Clear the Allow coarsening checkbox.
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Locate the Error Estimation section. In the table, enter the following settings:
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In the Model Builder window, expand the Results > Probe Plot Group 2 node, then click Probe Plot Group 2.
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In the Settings window for 1D Plot Group, type Relative Pressure Probes, Frequency Spectrum in the Label text field.
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Select the Frequency range checkbox.
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In the Settings window for 1D Plot Group, type Normalized Positive and Negative Pressure in the Label text field.
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In the Settings window for Line Graph, click Replace Expression in the upper-right corner of the y-Axis Data section. From the menu, choose Component 1 (comp1) > Nonlinear Pressure Acoustics, Time Explicit > Pressure and sound pressure level > nate.p_max - Maximum acoustic pressure - Pa.
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Locate the y-Axis Data section. In the Expression text field, type nate.p_max/at1(0, F, nate.p_max).
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In the Settings window for Line Graph, click Replace Expression in the upper-right corner of the y-Axis Data section. From the menu, choose Component 1 (comp1) > Nonlinear Pressure Acoustics, Time Explicit > Pressure and sound pressure level > nate.p_min - Minimum acoustic pressure - Pa.
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Locate the y-Axis Data section. In the Expression text field, type -nate.p_min/at1(0, F, nate.p_max).
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Locate the Legends section. In the table, enter the following settings:
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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) > Nonlinear Pressure Acoustics, Time Explicit > Cell time scale > nate.wtc - Cell wave time scale - s.
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