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In the Select Physics tree, select Structural Mechanics > Electromagnetics–Structure Interaction > Piezoresistivity > Piezoresistivity, Shell.
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Click Add.
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Browse to the model’s Application Libraries folder and double-click the file piezoresistive_pressure_sensor_shell_geom_sequence.mph.
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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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Click OK.
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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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In the Model Builder window, under Component 1 (comp1) > Shell (shell) click Thickness and Offset 1.
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In the Show More Options dialog, in the tree, select the checkbox for the node Physics > Advanced Physics Options.
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Click OK.
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In the Model Builder window, under Component 1 (comp1) > Electric Currents in Shells (ecis) click Conductive Shell 1.
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Locate the Coordinate System Selection section. From the Coordinate system list, choose Rotated System 2 (sys2).
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Locate the Coordinate System Selection section. From the Coordinate system list, choose Rotated System 2 (sys2).
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From the list, choose User-controlled mesh.
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Click the Custom button.
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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) > Shell > Displacement > shell.disp - Displacement magnitude - m.
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In the Settings window for 3D Plot Group, type In-Plane Shear Stress (Local Coordinates) in the Label text field.
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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) > Shell > Stress > Stress tensor, local coordinate system - N/m² > shell.slGp12 - Stress tensor, local coordinate system, 12-component.
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In the In-Plane Shear Stress (Local Coordinates) toolbar, click
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In the Settings window for Max/Min Surface, click Replace Expression in the upper-right corner of the Expression section. From the menu, choose shell.slGp12 - Stress tensor, local coordinate system, 12-component - N/m².
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In the Settings window for 1D Plot Group, type In-Plane Shear Stress (Local Coordinate System) 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) > Shell > Stress > Stress tensor, local coordinate system - N/m² > shell.slGp12 - Stress tensor, local coordinate system, 12-component.
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In the Settings window for Arrow Surface, click Replace Expression in the upper-right corner of the Expression section. From the menu, choose Component 1 (comp1) > Electric Currents in Shells > Currents and charge > ecis.JsX,...,ecis.JsZ - Surface current density (material and geometry frames).
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Locate the Expression section.
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Locate the Coloring and Style section.
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In the Settings window for Global Evaluation, click Replace Expression in the upper-right corner of the Expressions section. From the menu, choose Component 1 (comp1) > Electric Currents in Shells > Terminals > ecis.I0_1 - Terminal current - A.
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Click Add Expression in the upper-right corner of the Expressions section. From the menu, choose Component 1 (comp1) > Electric Currents in Shells > Terminals > ecis.V0_2 - Terminal voltage - V.
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Locate the Expressions section. In the table, enter the following settings:
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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 left checkbox.
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Select the Layers to the right checkbox.
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Select the Layers on top checkbox.
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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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Select the Layers to the left checkbox.
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Clear the Layers on bottom checkbox.
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Right-click Component 1 (comp1) > Geometry 1 > Work Plane 1 (wp1) > Plane Geometry > Rectangle 1 (r1) and choose Duplicate.
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Locate the Layers section. In the table, enter the following settings:
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Select the Keep input objects checkbox.
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In the Model Builder window, under Component 1 (comp1) > Geometry 1 right-click Work Plane 1 (wp1) and choose Virtual Operations > Form Composite Faces.
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On the object fin, select Boundaries 19, 20, 26–35, and 38 only.
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On the object cmf1, select Boundaries 11, 14–18, 25, 27, and 32–35 only.
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On the object cmf2, select Edges 24 and 94 only.
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Clear the Ignore adjacent vertices checkbox.
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On the object ige1, select Boundaries 7, 12, 15, 17, 21, and 24–26 only.
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On the object cmf3, select Edges 4, 6, 8, 12, 84, and 87–89 only.
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On the object ige2, select Boundary 9 only.
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On the object ige2, select Boundaries 3, 5, 6, 8, 13–15, and 18 only.
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Click OK.
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Click OK.
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Click
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Click OK.
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Click OK.
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Click OK.
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