All Courses
All Courses
Courses by Software
Courses by Semester
Courses by Domain
Tool-focused Courses
Machine learning
POPULAR COURSES
Success Stories
OBJECTIVE: 1. Perform Tetra mesh using Tetra4 elements for given housing Assembly. 2. Perform Hexa mesh using Hexa8 for given Arm bracket. 3. Perform calculations for stress wave propogation in steel rail and editing the RADIOSS Engine input file. TASK1: Tetra mesh using Tetra4 elements for given Housing Assembly:…
Siddhartha Shekhar
updated on 18 Jul 2021
OBJECTIVE:
1. Perform Tetra mesh using Tetra4 elements for given housing Assembly.
2. Perform Hexa mesh using Hexa8 for given Arm bracket.
3. Perform calculations for stress wave propogation in steel rail and editing the RADIOSS Engine input file.
TASK1:
Tetra mesh using Tetra4 elements for given Housing Assembly:
Imported CAD:
File>>Import>>Import Geometry>>STP file>>Open Import dialog box>>Choose step file>>OK>>Import.
Distributing assembly into different components:
Using Tool>>Organise>>Solids>>Choose>>Chhose compoenet>>Move.
Assemblies are divided into Outer and Inner components.
Outer component assembly
Inner component Assembly
Deleting Solids:
Solids are deleted to get the surface based volume mesh.
F2>Solids>>Displayed>OK
2D Tria mesh:
F12>>Choose surface>>Target element size = 5mm>>Choose element type = tria >>First order>>To current componet>>Mesh
3D - Tetra mesh:
Setting the Criteria file: Preference>>3D>>tet collapse = 0.15, this ensures element check threshhold.
Also, 3D>>Tetramesh>>Tetramesh parameters>>tet collapse = 0.15 so that generated mesh is as per this value.
Now, Tetra mesh >> Choose elems>>Simple pyramid>>elems to current component>>Mesh
By this we can convert the 2D tria mesh into 3D tetra4 mesh.
Checking the mesh volume: Using Mask elements we can see if volume mesh happened or not.
Fixing element quality:
Go to 3D>>Tetramesh>>Fix 3D elements>>Choose elems>>Choose criteria>>Enter value>>Show failed>>Fix.
Remaining elements can be corrected for tet collapse using Tools>>Translate.
Choose node>>Define plane>>Enter magnitude>>Translate + or translate -
Delete 2D shells:
At the end, delete all shell elements
F2>Elems>>by config>>quad4>Select entity>Delete
TASK2:
Hexa mesh using Hexa8 elements for given Arm bracket:
Imported CAD:
File>>Import>>Import Geometry>>STP file>>Open Import dialog box>>Choose step file>>OK>>Import.
Distributing assembly into different components:
Using Tool>>Organise>>Solids>>Choose>>Chhose compoenet>>Move.
Assemblies are divided into Outer and Inner components.
Base plate
Curve sleeve
Boss
Deleting Solids:
Solids are deleted to get the surface based volume mesh.
F2>Solids>>Displayed>OK
3D - Hexa mesh:
Setting the Criteria file: Preference>>3D>>Traget size = 5, this ensures element check threshhold.
Options for solid hex mapping:
However, Morphing can also be used to perform 3D hexa mesh.
Base plate using Solid Map
2D mesh with 10mm mesh on top face.
Using Tools>>Project>>Elems>>Surface>>surface normal>>project
now, 3D>>Solid map>>General>>Choose source elems>>Choose dest elems>>Choose along geometry (lateral surface)>>Enter density(5)>>Mesh
Arm sleeve using spin-part1:
Centre of nodes is found using F4>>three nodes>>Centre node.
Now, 3D>>Spin>>Spin elems (L shape base 2D shells are selected)>>3d elems faces by nodes>>Enter angle>>Spin elems>>Choose plan for circular spin>>Choose base>>mesh
Arm sleeve using spin-part2:
3D>>Linear solid>>Choose elems(from)>>choose elems(to)>>Assign alignment>>Density>>Solids
NOTE: Density of from and to elems should be same.
So, complete arm sleeve is:
Boss 3D mesh usinh Solid Map:
Based on the mesh density of associated elems from sleeve, we need to mesh on the Boss faces.
Now, 3D>>Solid map>>choose source elems>>choose destination elems>>along geometry (Node path with associated sleeve)>>mesh
this gives us the finish mesh for Boss
Final mesh:
Deleting quad4:
Delete all elems by config.
TASK3:
Calculation for the time step and modification in Engine input files:
From the Strater input file, we can get details about the Material used:
Youngs Modulus, E = 210000 MPa or N/mm2
Density,ρ = 0.0078 gm/mm3
speed of sound, c = √(E/ρ)
Speed of sound, c = √(210000/0.0078) mm/ms
c = 5188.7452 mm/ms
Length of rail, L = 1000 mm
Time taken, T = 1000 mm/ 5188.7452 mm/ms
T = 0.19272 ms
Modification in Engine input file:
Here, total termination time is T
and after every 0.02 ms animation file will be written.
Leave a comment
Thanks for choosing to leave a comment. Please keep in mind that all the comments are moderated as per our comment policy, and your email will not be published for privacy reasons. Please leave a personal & meaningful conversation.
Other comments...
Vehicle frontal crash for various cases - Simplified | FMVSS 208 Rigid Barrier, perpendicular, 100% Overlap at 56kmph. | ECE-R 94, Car to car frontal crash, 50% overlap at 50Kmph.
OBJECTIVE: To study the vehicle front crash. To understand the solver deck for this exercise. To understand the contacts, motion, and physics behind the vehicle crash. Output files associated with the practise. Correlation for Car crash with NCAP-36 load cell wall. DESIGN OF EXPERIMENT CASE 1: To understand…
20 Jul 2021 02:29 AM IST
Assignment 2-RADIOSS Engine File Editing & 3D Meshing Challenge
OBJECTIVE: 1. Perform Tetra mesh using Tetra4 elements for given housing Assembly. 2. Perform Hexa mesh using Hexa8 for given Arm bracket. 3. Perform calculations for stress wave propogation in steel rail and editing the RADIOSS Engine input file. TASK1: Tetra mesh using Tetra4 elements for given Housing Assembly:…
18 Jul 2021 01:25 AM IST
Assignment 1-2D Meshing Challenge
OBJECTIVE: For the given three parts, carry out the following: Geometry Clean-up Extracting the Midsurface Midsurface clean up Defeaturing the holes < 5mm 2D quad mesh with target element length 5mm Property assignement to assign thickness. PART1: Fig1: Imported Model. Geometry Clean-up fig2: Wireframe…
15 Jul 2021 10:24 PM IST
Solution of a load-displacement non linear relation for static analysis using Explicit and Implicit method in MS Excel using VBA programming
OBJECTIVE: For a given non linear relation between load and displcement where load is defined as a function of displacement. F(u) = u3 + 9u2 + 4u Solve the above relation for static analysis using Implicit and Explicit scheme. DESIGN OF EXPERIMENT: Loading is done in the increements of 1.0 N with…
14 Jul 2021 03:20 PM IST
Related Courses
Skill-Lync offers industry relevant advanced engineering courses for engineering students by partnering with industry experts.
© 2025 Skill-Lync Inc. All Rights Reserved.