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Shell Idealization Over the Solid Model in Geometric Element Analysis

PARTHIBAN_K
16-Pearl

Shell Idealization Over the Solid Model in Geometric Element Analysis

Shell Idealization Over the Solid Model in Geometric Element Analysis

Hello Guys,

Here, I am going to explain about the advantages of shell idealization over the solid model. I have done Geometric Element Analysis on sheet metal bracket using Creo Simulate (Pro Mechanica)

I have considered 2 cases, one for the sheet metal bracket with the 3D solid model and another one for the same component of 2D Shell model.

1.BOUNDARY CONDITIONS

Following Boundary Conditions and Design Considerations are taken for the analysis

Units

S.NOUnitValue
1.LengthMm
2.MassKg
3.TimeSec
4.TemperatureC

Material Details

S.NODescriptionValue
1.MaterialSteel
2.Density7.83*10^-06 Kg/mm^3
3.Young’s Modulus200 GPa
4.Poisson’s Ratio0.27
5.SymmetryIsotropic

Sheet Metal Bracket

Model

The drawing details of the model Considered for this analysis

Load

Uniformly distributed Load  of 100 Kg applied on loading area (mentioned in the figure)

Constraints

All the Degree Of Freedom fixed at the M8 tap hole (mentioned in the figure)

2. MESHING

In Creo Simulate, the default solver is Auto GEM, which uses p-method to solve the model i.e. It uses the highest polynomials order of each element to solve the element equation instead of changing the number of elements (like FEA method) i.e. it changing the element shape to get the better result. That’s why Creo Simulate also called Geometric Element Analysis (GEA) application.

Case 1: Mesh – Sheet Metal 3D Solid Model

In this case, the model considered as solid. The model meshed with the Auto GEM option with the maximum element size of 6 mm.

Solid Model meshed with CREO Auto GEM

Solid Model meshed with CREO Auto GEM

Auto GEM created totally 8689 Tetrahedron elements on Solid Model in 0.03 minutes.

Case 2: Mesh – Sheet Metal 2D Shell Idealized

In this case, thin mid-shell made on the solid model using shell pair option in the Creo Simulate & meshing done with the Auto GEM

Shell Model meshed using CREO Auto GEM

Shell Model meshed using CREO Auto GEM

Auto GEM created totally 248 triangular & 664 Quadrilateral elements in Shell Model in less than 0.01 minutes

Solid Mesh Vs Shell Mesh

This chart shows the difference of meshing operation between the 3D Solid model & the 2D Shell model

Mesh Comparison between 3D solid model vs 2d shell model

Mesh Comparison between 3D solid model vs 2d shell model

From the chart, it clearly shows solid model takes more time for meshing than shell model because it creates large number of 3D elements while the shell model requires less number of 2D elements.

here the 3D Solid model takes nearly 10 times more elements then 2D Shell model.

3.RESULT COMPARISON

These figure shows the difference between displacement analysis of solid and shell model. The result variation between both cases are less than 1%.

3D SOLID MODEL - DISPLACEMENT ANALYSIS

3D SOLID MODEL – DISPLACEMENT ANALYSIS

2D SHELL MODEL - DISPLACEMENT ANALYSIS

2D SHELL MODEL – DISPLACEMENT ANALYSIS

From the analyzed result the deformed magnitude displacement of the solid model is 2.44 mm and the shell model is 2.49 mm. The variation in result between the both cases are very low.

I have generated following charts to understand the difference between both cases

Displacement Variation between 3D Solid model vs 2D Shell Model

Displacement Variation between 3D Solid model vs 2D Shell Model

Total analysis takes 7.65 seconds for the shell model and 24.42 seconds for the solid model. The disk space consumed by the solid model is 175 Mb and the shell mode is 35 Mb

Time & Disk space consumption between 3D Solid & 2D Shell Model

Time & Disk space consumption between 3D Solid & 2D Shell Model

OBSERVED ADVANTAGES

  1. The 2D Shell model of the component takes less time to mesh comparatively the 3D Solid model of the same component
  2. Displacement result varies less than 1% between the 2D shell model & the 3D solid model of the same component
  3. The 3D solid model of the component nearly consumes  3 times more TIME than the 2D shell model of the same component
  4. The 3D solid model of the component requires nearly 5 times more disk space than the 2D shell model of the same component

LIMITATION

  1. The 2d Shell model only applicable for the model with symmetric projection from the midplane like Sheet Metal Components.
  2. Not suitable for Non-Linear analysis such as Large deformation & contact.

( Paul Kloninger‌ suggested)


CONCLUSION

Creo Simulates (Pro Mechanica) provides the powerful option Shell pair for extracting mid-plane from the solid model. Analysis with the mid-plane efficiently savings the time taken and the disk space for an analysis.

See more articles in my blog

http://jkparthiban.com/index.php/category/all/


Parthiban Kannan

href="https://www.linkedin.com/in/parthiban-kannan/" target="_blank"
6 REPLIES 6

Shell model...

Contact???

Large Deformation???

not possible

support / example

example.jpg

Hi, Paul Kloninger

  Nice Job, We can add the contact & large deformation to Limitations of shell model. also, u have used the symmetry feature from Simulate that too have some more advantages than using full model.

Thank you for your valuable Job.

Parthiban Kannan

href="https://www.linkedin.com/in/parthiban-kannan/" target="_blank"

Hi, in the drawing is missing some measures like inner and outer radius.

I'm trying to redo the exercise with solid non-tetra elements.

What about in modal analysis? Are the natural frequencies within 5% as your static deflection results?

Thanks in advance.

Rich Hilson

 

A short test for Modal Analyses with only solid versus Solid AND shell in Creo 5.0.2.0. Strangly calculation time is MUCH MORE with shells than with only Solid in this case (49min. vs 1min). Mesh settings are default and only Quickstudy is applied, so I wouldn't worry over the result difference. I'm not ready to jump into conclusions yet, but at least be alert using shells in Modal.

C5_solid_vs_shell_modal.jpg

We found Modal Analyses (in this example) is only slow when using Shell Pairs, not with 'simple' shells (defined by a single surface).

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