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Click Add.
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In the Select Physics tree, select Acoustics > Pressure Acoustics > Pressure Acoustics, Frequency Domain (acpr).
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Click Add.
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Click Add.
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Click
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In the Select Study tree, select Preset Studies for Some Physics Interfaces > Coil Geometry Analysis.
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Click
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Click
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Browse to the model’s Application Libraries folder and double-click the file loudspeaker_driver_3d_parameters.txt.
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Click
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Browse to the model’s Application Libraries folder and double-click the file loudspeaker_driver_3d.mphbin.
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Click
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Select the Group by continuous tangent checkbox.
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Go to the Add Material window.
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Click the Add to Component button in the window toolbar.
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Click the Add to Component button in the window toolbar.
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Click the Add to Component button in the window toolbar.
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In the Material Browser window, In the ribbon make sure to select the Materials tab and then click the Browse Materials icon.
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click
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Browse to the model’s Application Libraries folder and double-click the file loudspeaker_driver_materials.mph.
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Click
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In the Model Builder window, under Component 1 (comp1) > Materials click Soft Iron (With Losses) (mat2).
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Locate the Material Contents section. In the table, enter the following settings:
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Locate the Constitutive Relation Jc-E section. From the σ list, choose User defined. In the associated text field, type 5[S/m].
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Locate the Constitutive Relation B-H section. From the Magnetization model list, choose Remanent flux density.
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Specify the e vector as
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Locate the Constitutive Relation Jc-E section. From the σ list, choose User defined. In the associated text field, type 5[S/m].
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From the list, choose User defined.
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In the Model Builder window, expand the Component 1 (comp1) > Magnetic Fields (mf) > Domain Coil 1 > Geometry Analysis 1 node, then click Geometry Analysis 1.
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In the Model Builder window, under Component 1 (comp1) click Pressure Acoustics, Frequency Domain (acpr).
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In the Settings window for Pressure Acoustics, Frequency Domain, locate the Domain Selection section.
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In the Settings window for Exterior Field Calculation, locate the Exterior Field Calculation section.
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Click
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In the Model Builder window, under Component 1 (comp1) > Solid Mechanics (solid) click Linear Elastic Material 1.
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In the Physics toolbar, click
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In the Model Builder window, under Study 1 - Frequency Response click Step 1: Coil Geometry Analysis.
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Clear the Include geometric nonlinearity checkbox.
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In the Solve for column of the table, under Component 1 (comp1), clear the checkbox for Solid Mechanics (solid).
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In the Solve for column of the table, under Component 1 (comp1) > Multiphysics, clear the checkbox for Magnetomechanics, Solid 1 (mmcpl1).
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In the Study toolbar, click
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Click
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Click Replace.
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Click the Custom button.
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Locate the Element Size Parameters section. In the Maximum element size text field, type 343[m/s]/fmax/5.
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Click the Custom button.
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Locate the Element Size Parameters section.
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Click the Custom button.
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Locate the Element Size Parameters section.
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Click the Custom button.
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Locate the Element Size Parameters section.
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Click the Custom button.
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Locate the Element Size Parameters section.
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In the Model Builder window, expand the Study 1 - Frequency Response > Solver Configurations > Solution 1 (sol1) > Stationary Solver 3 node.
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4
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Right-click Study 1 - Frequency Response > Solver Configurations > Solution 1 (sol1) > Stationary Solver 3 > Suggested Iterative Solver (GMRES with GMG) (asb1_mmcpl1) and choose Enable.
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5
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Go to the Add Study window.
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Find the Studies subsection. In the Select Study tree, select Preset Studies for Selected Multiphysics > Eigenfrequency.
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Click the Add Study button in the window toolbar.
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Locate the Physics and Variables Selection section. In the Solve for column of the table, under Component 1 (comp1), clear the checkboxes for Magnetic Fields (mf) and Pressure Acoustics, Frequency Domain (acpr).
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5
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In the Solve for column of the table, under Component 1 (comp1) > Multiphysics, clear the checkboxes for Acoustic–Structure Boundary 1 (asb1) and Magnetomechanics, Solid 1 (mmcpl1).
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Locate the Data section. From the Dataset list, choose Study 1 - Frequency Response/Solution Store 2 (sol3).
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Click Define custom colors.
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Click Add to custom colors.
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Click Define custom colors.
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Click Add to custom colors.
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Click Define custom colors.
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Click Add to custom colors.
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Click Define custom colors.
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Click Add to custom colors.
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Locate the Data section. From the Dataset list, choose Study 1 - Frequency Response/Solution Store 2 (sol3).
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Click OK.
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Select the Radius scale factor checkbox.
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Select the Radius scale factor checkbox.
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Click
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4
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In the Paste Selection dialog, type 12-23, 27, 28, 31-36, 38, 39, 63-67, 69, 70, 92, 93, 95, 96, 102, 103, 106-108, 119-123, 132, 133, 142, 147-151, 153, 154, 159-161, 258-260, 276-279, 282, 284-287, 289, 301-303, 305, 317, 319, 323, 325, 326, 332-334, 352, 357, 360-363, 366 in the Selection text field.
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Click OK.
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Click
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4
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In the Paste Selection dialog, type 11, 12, 14, 20, 85, 88, 90-92, 94, 110, 112, 132, 174, 190-192, 198, 199, 205 in the Selection text field.
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Click OK.
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Select the Compute differential checkbox.
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Select the Compute differential checkbox.
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Select the Compute differential checkbox.
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Locate the Plot Settings section.
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Locate the Plot Settings section.
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Go to the Result Templates window.
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3
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In the tree, select Study 2 - Structural Eigenmodes/Solution 4 (sol4) > Solid Mechanics > Mode Shape (solid).
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4
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Click the Add Result Template button in the window toolbar.
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Click
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4
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Browse to the model’s Application Libraries folder and double-click the file loudspeaker_driver_2d.mphtxt.
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5
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Click
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6
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Click
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1
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Click
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4
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Browse to the model’s Application Libraries folder and double-click the file loudspeaker_driver_3d_polygon1_coordinates.txt.
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Click OK.
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Click OK.
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Click OK.
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Click OK.
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On the object pare1, select Point 25 only.
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On the object pare1, select Point 23 only.
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On the object pare1, select Point 13 only.
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5
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On the object pare1, select Point 14 only.
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Click the Angles button.
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Click OK.
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On the object del1, select Edges 217, 218, 220, 222, 224, 227, 362–366, and 368 only.
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5
|
Click OK.
|
|
6
|
|
1
|
|
2
|
|
3
|
On the object pare1, select Point 199 only.
|
|
4
|
|
5
|
|
6
|
On the object pare1, select Point 201 only.
|
|
1
|
|
2
|
On the object pare1, select Point 188 only.
|
|
3
|
|
4
|
|
5
|
On the object pare1, select Point 198 only.
|
|
1
|
|
2
|
On the object pare1, select Point 111 only.
|
|
3
|
|
4
|
|
5
|
On the object pare1, select Point 112 only.
|
|
1
|
|
2
|
On the object pare1, select Point 154 only.
|
|
3
|
|
4
|
|
5
|
On the object pare1, select Point 158 only.
|
|
1
|
|
2
|
|
3
|
|
4
|
|
5
|
Click OK.
|
|
1
|
|
2
|
|
3
|
|
4
|
|
5
|
Click OK.
|
|
1
|
|
2
|
|
3
|
|
4
|
|
5
|
Click OK.
|
|
6
|
|
7
|
|
8
|
|
1
|
|
2
|
On the object thi1, select Edges 9, 14, 20, 26, 27, 37, 39, and 44 only.
|
|
3
|
|
4
|
|
1
|
|
2
|
|
3
|
|
4
|
|
5
|
|
6
|
|
7
|
|
1
|
|
2
|
|
3
|
|
4
|
|
5
|
Click OK.
|
|
6
|
|
7
|
Select the Keep input objects checkbox.
|
|
1
|
|
2
|
|
3
|
|
4
|
On the object cyl1, select Domain 1 only.
|
|
1
|
|
2
|
On the object fin, select Domains 1, 7, 20, 21, 23, 31, and 37 only.
|
|
1
|
|
2
|
|
3
|
|
4
|
In the Paste Selection dialog, type 145,146,155,186,212,214,216,218,224,231,234,235 in the Selection text field.
|
|
5
|
Click OK.
|
|
1
|
|
2
|
On the object cmf1, select Boundaries 149, 181, 184, 217, 219, and 227 only.
|
|
1
|
|
2
|
On the object cmf2, select Domains 30, 32, and 33 only.
|