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Modeling a composite laminated shell requires a 2D surface geometry, called a base surface, and a Layered Material node that adds an extra dimension (1D) to the base surface geometry in the surface normal direction. Using the Layered Material functionality, you can model several layers of different thicknesses, material properties, and fiber orientations. You can optionally specify the interface materials between the layers and the control mesh elements in each layer.
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The Layered Material Stack node is used to define various zones/sections of the piezoresistive pressure sensor.
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The third direction for the selected coordinate system in the Single Layer Material, Layered Material Link, or Layered Material Stack represents the normal direction of the Layered Shell or Shell physics. This is also the direction in which the layer stacking is interpreted from bottom to top, and therefore, it is crucial to know it during modeling. There are two ways to achieve this:
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Using physics symbols: Go to the physics settings, find the Physics Symbols section, and select the Enable physics symbols checkbox. Then go to the material feature, for instance, Linear Elastic Material, to see the normal direction represented by green arrows in the geometry.
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Using result templates: When a solution dataset is available, use the result template Thickness and Orientation to plot the normal direction.
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To visualize the results as a 3D solid object, you can use the Layered Material dataset, which creates a virtual 3D solid object combining the surface geometry (2D) and the extra dimension (1D).
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In the Select Physics tree, select Structural Mechanics > Electromagnetics–Structure Interaction > Piezoresistivity > Piezoresistivity, Layered 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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Select the Group by continuous tangent checkbox.
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On the object ige2, select Boundaries 1–18 only.
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Drag and drop below Membrane (boxsel1).
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Click
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Click Build Preceding State.
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Click OK.
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Find the Coordinate names subsection. From the Create first tangent direction from list, choose Rotated System 2 (sys2).
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Go to the Add Material window.
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Click the Add to Global Materials button in the window toolbar.
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Click the Add to Global Materials button in the window toolbar.
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Locate the Layer Definition section. In the table, enter the following settings:
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Locate the Layer Definition section. In the table, enter the following settings:
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In the Settings window for Layered Material Stack, click Layer Cross-Section Preview in the upper-right corner of the Layered Material Settings section. From the menu, choose Create Layer Cross-Section Plot.
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In the Model Builder window, expand the Results node, then click Component 1 (comp1) > Layered Shell (lshell) > Linear Elastic Material 1.
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In the Model Builder window, under Component 1 (comp1) click Electric Currents in Layered Shells (ecis).
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In the Settings window for Electric Currents in Layered Shells, locate the Boundary Selection section.
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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 to show model input sections.
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In the Model Builder window, under Component 1 (comp1) > Electric Currents in Layered Shells (ecis) click Conductive Shell 1.
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From the list, choose User-controlled mesh.
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Click
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Clear the Generate default plots checkbox.
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Click
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Click OK.
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Go to the Result Templates window.
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Click the Add Result Template button in the window toolbar.
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Click the Add Result Template button in the window toolbar.
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In the tree, select Study 1/Solution 1 (1) (sol1) > Electric Currents in Layered Shells > Electric Potential (ecis).
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Click the Add Result Template button in the window toolbar.
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Select the Show maximum and minimum values checkbox.
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Select the Show maximum and minimum values checkbox.
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In the Settings window for 1D Plot Group, type In-Plane Shear Stress along Diaphragm Edges in the Label text field.
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Locate the Plot Settings section.
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Select the y-axis label checkbox. In the associated text field, type Stress tensor, local coordinate system, 12-component (MPa).
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Select the Radius scale factor checkbox.
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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 Layered 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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Go to the Result Templates window.
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In the tree, select Study 1/Solution 1 (1) (sol1) > Layered Shell > Geometry and Layup (lshell) > Shell Geometry (lshell).
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Click the Add Result Template button in the window toolbar.
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Drag and drop below Layer Cross-Section Preview.
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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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