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General Flexible Plate

Thin plate with elastic properties for deformation

  • Library:
  • Simscape / Multibody / Body Elements / Flexible Bodies / Plates and Shells

  • General Flexible Plate block

Description

The General Flexible Plate block models thin, flat structure capable of elastic deformations, including stretch, bending, and shear effects. The block applies the shear deformation Mindlin plate theory [1][2][3] and uses the finite element method [4] for its solution. You can use this block to model thin, flat structures, such as linkages and satellite solar panels.

General Flexible Plate

To specify the geometry of a plate, use the Midsurface and Thickness parameters. The midsurface of the plate is in the xy plane and the thickness is along the z axis. The thickness must be much smaller than the width and length of the plate, and the plate is symmetric about the midsurface. See the Geometry section for more details.

The block models a flexible plate made of homogeneous, isotropic, and linearly elastic materials. You can specify the density, Young's modulus, and Poisson's ratio or shear modulus of the plate in the Stiffness and Inertia section. Additionally, the block supports two damping methods to control the performance of the modeling. To add custom frames to the plate, specify parameters in the Frames section.

Ports

Frame

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Custom body-attached frames. Specified the name of the port using the New Frame parameter. If you do not specify the name of the custom frame, the block names the frame FN, where N is an identifying number.

Dependencies

To enable a custom frame port, create a frame by clicking New Frame.

Parameters

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Geometry

Coordinates used to specify the midsurface boundaries of the plate on the local xy plane. You can specify the midsurface by using:

  • An N-by-2 matrix of xy coordinates to specify a midsurface. Each row gives the [x,y] coordinates of a point on the mid-surface boundaries. The points connect in the specified order to form a closed polyline. To ensure that the polyline is closed, the block inserts a line segment between the last and first points.

  • An M-by-1 or 1-by-M cell array of N-by-2 matrices of xy coordinates to specify a midsurface with holes. The first element in the array represents the outer boundary and subsequent elements specify the hole boundaries.

Note

Ensure that any two boundaries do not intersect, overlap, or touch.

Additionally, each individual boundary must have:

  • No repeated vertices

  • No self-intersections

  • At least three non-collinear points

Thickness of the plate. The block models the plate by extruding the specified midsurface along the local z axis of the plate. The extrusion is symmetric about the local xy plane of the pate. The thickness should be much smaller than the overall midsurface dimensions for plate theory to apply.

Stiffness and Inertia

Mass per unit volume of material. The default value corresponds to aluminum.

Elastic properties used to parameterize the plate. You can specify either Young's Modulus and Poisson's Ratio or Young's and Shear Modulus. These properties are commonly available in materials databases.

Young's modulus of the elasticity of the plate. The greater the value of this parameter, the stronger the resistance to bending and in-plane normal deformation. The default value corresponds to aluminum.

Poisson's ratio of the plate. The value specified must be greater than or equal to 0 and smaller than 0.5. The default value corresponds to aluminum.

Dependencies

To enable this parameter, set Specify to Young's Modulus and Poisson's Ratio.

Shear modulus, also known as the modulus of rigidity, of the plate. The larger value correlates to a stronger resistance to shearing and twisting. The default value corresponds to aluminum.

Dependencies

To enable this parameter, set Specify to Young's and Shear Modulus.

Damping

Damping method for the plate:

  • Select None to model undamped plates.

  • Select Proportional to apply the proportional (or Rayleigh) damping method. This method defines the damping matrix [C] as a linear combination of the mass matrix [M] and stiffness matrix [K]:

    [C]=α[M]+β[K],

    where α and β are the scalar coefficients.

  • Select Uniform Modal to apply the uniform modal damping method. This method applies a single damping ratio to all the vibration modes of the plate. The larger the value, the faster vibrations decay.

Coefficient α of the mass matrix. This parameter defines damping proportional to the mass matrix [M].

Dependencies

To enable this parameter, set Type to Proportional.

Coefficient β of the stiffness matrix. This parameter defines damping proportional to the stiffness matrix [K].

Dependencies

To enable this parameter, set Type to Proportional.

Damping ratio ζ applied to all vibration modes of a plate. The larger the value, the faster vibrations decay. The vibration modes are underdamped if ζ < 1 and overdamped if ζ > 1.

Dependencies

To enable this parameter, set Type to Uniform Modal.

Data Types: double

Graphic

Graphic used to visualize the plate. To hide the plate in the Mechanics Explorer, set this parameter to None.

Parameterization for specifying visual properties. Select Simple to specify color and opacity. Select Advanced to specify more visual properties, such as Specular Color, Ambient Color, Emissive Color, and Shininess.

Dependencies

To enable this parameter, set Type to From Geometry.

RGB color vector with red (R), green (G), and blue (B) color amounts specified on a 0–1 scale. You can also specify a color by using the color picker.

Dependencies

To enable this parameter, set:

  1. Type to From Geometry

  2. Visual Properties to Simple

Graphic opacity, specified on a scale of 0–1. An opacity of 0 corresponds to a completely transparent graphic and an opacity of 1 to a completely opaque graphic.

Dependencies

To enable this parameter, set:

  1. Type to From Geometry

  2. Visual Properties to Simple

Color of the graphic under direct white light, specified as an [R G B] or [R G B A] vector on a 0–1 scale. The optional fourth element specifies the color opacity on a scale of 0–1. Omitting the opacity element is equivalent to specifying a value of 1.

Dependencies

To enable this parameter, set:

  1. Type to From Geometry

  2. Visual Properties to Advanced

Color of the specular highlights, specified as an [R,G,B] or [R,G,B,A] vector on a 0–1 scale. The optional fourth element specifies the color opacity. Omitting the opacity element is equivalent to specifying a value of 1.

Dependencies

To enable this parameter, set:

  1. Type to From Geometry

  2. Visual Properties to Advanced

Color of shadow areas in diffuse ambient light, specified as an [R,G,B] or [R,G,B,A] vector on a 0–1 scale. The optional fourth element specifies the color opacity. Omitting the opacity element is equivalent to specifying a value of 1.

Dependencies

To enable this parameter, set:

  1. Type to From Geometry

  2. Visual Properties to Advanced

Surface color due to self illumination, specified as an [R,G,B] or [R,G,B,A] vector on a 0–1 scale. The optional fourth element specifies the color opacity. Omitting the opacity element is equivalent to specifying a value of 1.

Dependencies

To enable this parameter, set:

  1. Type to From Geometry.

  2. Visual Properties to Advanced.

Sharpness of the specular light reflections, specified as a scalar number on a 0–128 scale. Increase the shininess value for smaller but sharper highlights. Decrease the value for larger but smoother highlights.

Dependencies

To enable this parameter, set:

  1. Type to From Geometry

  2. Visual Properties to Advanced

Frames

Click the Create button Create to open a pane for creating a new body-attached frame. In this pane, you can specify the name, origin, and orientation for the frame.

  • To name the custom frame, enter a name in the Frame Name parameter. The name identifies the port on the block and in the tree view pane of the Mechanics Explorer.

  • Select a frame origin in the Frame Origin section:

    • At Reference Frame Origin: Make the new frame origin coincident with the origin of the reference frame of the undeformed plate.

    • Based on Geometric Feature: Make the new frame origin coincident with the center of the selected undeformed geometry feature. Valid features include surfaces, lines, and points. Select a feature from the visualization pane, then click Use Selected Feature button to confirm the location of the origin. The name of the origin location appears in the field below this option.

  • To define the orientation of the custom frame, under the Frame Axes section, select the Primary Axis and Secondary Axis of the custom frame and then specify their directions.

    Use the following methods to select a vector for specifying the directions of the primary and secondary axes. The primary axis is parallel to the selected vector and constrains the remaining two axes to its normal plane. The secondary axis is parallel to the projection of the selected vector onto the normal plane.

    • Along Reference Frame Axis: Selects an axis of the reference frame of the undeformed plate.

    • Based on Geometric Feature: Selects the vector associated with the chosen geometry feature of the undeformed plate. Valid features include surfaces and lines. The corresponding vector is indicated by a white arrow in the visualization pane. You can select a feature from the visualization pane and then click Use Selected Feature button to confirm the selection. The name of the selected feature appears in the field below this option.

Frames that you created. Specified the name of the port using the New Frame parameter. If you do not specify the name of the custom frame, the block names the frame FN, where N is an identifying number.

  • Click the text field to edit the name of an existing custom frame.

  • Click the Edit button Edit to edit other aspects of the custom frame, such as the origin and axes.

  • Click the Delete button Delete to delete the custom frame.

Dependencies

To enable this parameter, create a frame by clicking New Frame.

References

[1] Bathe, Klaus-Jürgen. Finite Element Procedures. 2nd ed. Englewood Cliffs, N.J: Prentice-Hall, 2014.

[2] Cook, Robert Davis. Concepts and Applications of Finite Element Analysis. 4th ed. New York, NY: Wiley, 2001.

[3] Dvorkin, Eduardo N., and Klaus‐Jürgen Bathe. “A Continuum Mechanics Based Four‐node Shell Element for General Non‐linear Analysis.” Engineering Computations 1, no. 1 (January 1984): 77–88. https://doi.org/10.1108/eb023562.

[4] Bucalem, M. L., and K. J. Bathe. “Finite Element Analysis of Shell Structures.” Archives of Computational Methods in Engineering 4, no. 1 (March 1997): 3–61. https://doi.org/10.1007/BF02818930.

Extended Capabilities

C/C++ Code Generation
Generate C and C++ code using Simulink® Coder™.

Introduced in R2021b