Shell (2-D) Meshing Of A Car Hood
Shell (2-D) Meshing Of A Car Hood
Aim: To create the shell (2-D) meshing for a car hood model by eliminating geometrical errors and considering the given element quality criteria using ANSA.
Element Quality Criteria:
| S.No | Quality Criteria | Value |
| 1 | Target/Average length | 5 |
| 2 | Minimum Length | 3 |
| 3 | Maximum Length | 7 |
| 4 | Aspect | 3 |
| 5 | Warpage | 15 |
| 6 | Skewness | 45 |
| 7 | Jacobian | 0.7 |
| 8 | Minimum Quad Angle | 45 |
| 9 | Maximum Quad Angle | 135 |
| 10 | Minimum Tria Angle | 30 |
| 11 | Maximum Tria Angle | 120 |
| 12 | Tria Percentage | 15 |
Procedure:
The meshing is done by following steps
1. Import Hood.stp in to the ANSA
2. CAD Geometry clean up and topology
3. Mid-surface extraction
4. Setting the PID
5. Defeaturing
6. Shell meshing
1. Import Hood.stp in to the ANSA: Import the given Hood model_1.stp in to the ANSA Shown in the fig.1.1 and make orientation of all visual faces show in fig.1.2a, fig.1.2b and 1.2c for outer panel, inner panel and latches respectively.
Fig.1.1: Imported File
Fig.1.2a: Outer Panel
Fig.1.2a: Inner Panel
Fig.1.2c: Latches
2. CAD Geometry clean up and topology: In this step the given model undergo geometry check (Tools>Checks>Geometry) where ANSA check for any geometrical errors such as collapsed faces, cracks, single con, triple con etc. those errors are shown in fig. 2.1.
Fig.2.1: Geometry Errors
Geometrical errors are cleared by using release triple cons and topo, deleting the overlapped faces and creating new faces. fig.2.2 shows the fixed all Geometrical errors.
Fig.2.2: Geometry Clean Up
Before going to the Mid-surface check geometrical errors for all individual.
3. Mid-surface extraction: the given model has all sheet metal parts and Before going to the Mid surface extraction make a note for thickness of all parts (Utilities>Measure).
| S.No | Name | Thickness (mm) |
| 1 | Outer Panel | 0.75 |
| 2 | Inner Panel | 0.75 |
| 3 | Latches | 1.2 |
Mid-surface extraction done by manually because it is easy to extract. We can retain all CAD surfaces. Due to CAD surfaces we can easily conclude mid-surface position By comparing with it. Where as in auto mid-surface it is difficult to retain CAD surfaces.
Here mid-Surface extracted by Offset method (Topo>Faces>Offset>Faces) shown in the fig.3.1.
Fig.3.1: Mid-Surface Extraction by Offset
While extracting the mid-surface by Offset method it will ask for the offset distance along with direction. With respect to direction input the value. The value may be +ve or -ve depending on direction shown in the fig.3.2.
Fig.3.2: Offset Method
Mid-surface extracted for all parts shown in the fig.3.3a, 3.3b and 3.3c.
Fig.3.3a: Outer panel Mid-Surface
Fig.3.3b: Inner panel Mid-Surface
Fig.3.3c: Latches Mid-Surface
4. Setting the PID: setting PID (Property ID) for each mid surface done by using Set PID (Topo>Faces>Set PID). ANSA asked to select faces after conforming the faces Property Help window will pop up, in that window create new PID by right clicking mouse button and select New>PSHELL. Another PSHELL window will popup there we can assign the Name, MID (material ID) and thickness shown in the fig.4.1. We can modify the colors of each PID.
Fig.3.3c: Setting The PID
5) Defeaturing: Update the element length as per given element Quality criteria (Mesh>Perimeters>Length) which is Target/Average length 5. Removing all unnecessary edges, fillet radiuses etc. also maintain distance between two cons or nodes not less than Minimum Length of 3. Before and after defeaturing for outer panel, inner panel and latches shown in the fig.5.1, 5.2 and 5.3 respectively.
Fig.5.1: Outer Panel
Fig.5.2: Inner Panel
Fig.5.2: Latches
6. Shell Meshing: Assign given element Quality criteria in to the ANSA (Utilities>Quality criteria) and Mesh Parameters (Utilities>Mesh Parameters) shown in Fig.6.1. Here we are going to Generate Shell Mesh which is preferred for 2D mesh.
Fig.6.1: Quality Criteria & Mesh Parameters
Start meshing Process by Best Mesh (MESH>Mesh Generation>Best).
Modify mesh flow using Reconstruct (MESH>Shell Mesh>Reconstruct), Smooth (MESH>Shell Mesh>Smooth) and Split (MESH>Elements>Split). Make sure that while doing mesh all the element Quality criteria mush satisfied. Avid maxium opposite trais and quad elements.
In fig.6.2, 6.3 and 6.4 show the mesh flow.
Fig.6.2: Outer Panel Mesh Flow
Fig.6.3: Inner Panel Mesh Flow
Fig.6.4: latches Mesh Flow
Thickness assigned to the all parts by selecting Draw Shell As Solid (Utilities>Quality criteria>Presentation Parameters) and shown on the fig.6.5, fig.6.6, Ans fig.6.7.
Fig.6.5: Outer Panel Thickness
Fig.6.6: Inner Panel Thickness
Learning Outcome:
- Learnt user inter face of ANSA.
- Learnt CAD geometry clean up, topology, Mid-surface extraction And Defeaturing.
- Learnt shell meshing and making good mesh flow with considering the Quality criteria
Conclusion
Shell (2-D) mesh is done Successfully for a car hood model by eliminating geometrical errors and considering the given element quality criteria using ANSA.
(Find the attached file of Hood model_Complete_mesh.stp)