ICEMCFD Hexa meshing Advanced Level Course
- Description
- Curriculum
- FAQ
- Reviews
Meshing is the process to divide the continuous domain into discrete parts to solve fluid dynamics equation to get solution of flow field and heat transfer numerically on computers. ICEMCFD is one of the leading meshing software and it is specially best for getting high quality hexa meshing for accurate CFD results.
In this course you will learn to create high quality hexa mesh with 15 high quality workshops / cases in different applications areas. You will learn to use ICEMCFD options effectively to create the blocking and also you will be able to think about the blocking strategy yourself.
Workshops/cases covered in this course are:
Workshop 1 : Geometry, domain and hexa meshing of NACA 0012 3D airfoil with different trailing edges and domain shapes.
Workshop 2 : Hexa meshing of Square Duct
Workshop 3 : Hexa meshing of cube in external flow
Workshop 4 : Hexa meshing technique for quarter cylinder
Workshop 5 : Hexa meshing of vortex generator over ramp
Workshop 6 : Transition piping hexa mesh
Workshop 7 : Hexa meshing of two type of hemispheres configuration for external flow analysis
Workshop 8 : Hexa meshing Ventrui scruber with three nozzles at throat area
Workshop 9 : 3D injection nozzle system for coal, air and straw
Workshop 10 : Hexa meshing Gas Turbine Combustion Chamber
Workshop 11 : Hexa meshing of Supersonic Converging-Diverging Nozzle with Far Filed
Workshop 12 : Hexa meshing of U-Bend with top-down and bottom-up approaches
Workshop 13 : Hexa meshing of simple dimple over flat surface
Workshop 14 : Hexa meshing of triple wedge in supersonic external flow
Workshop 15 : Hexa meshing of of cone with different blocking approaches
Note: This course requires some basic knowledge on ICEMCFD. Some basic courses you can also find on udemy to start with.
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2Introduction
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3Layout of workshop and important files
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4Creating NACA 0012 airfoil and domain from coordinates
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5Creating circular domain and square trailing edge from previous model
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6Creating 3D domain from 2D geometry in ICEMCFD and part names
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7Geometry files for all four cases
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8Blocking strategy for case 1 : Rectangular domain with sharp TE airfoil
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9Blocking splitting, block collapse and association to airfoil
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10Blocking adjustment in tip region
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11O-Grid and Y-Grid in tip region
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12Pre-mesh on airfoil & domain and using scan plans to inspect mesh
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13Blocking optimization, quality check and mesh export for Case 1
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14Another blocking approach for tip region for Case 1
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15Case 2 : Blocking approach and key features
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16Case 2 : Tip region - Similar approach as of case 1
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17Blocking approach for case 3
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18Blocking approach for case 4
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19Moving 3D Airfoil by 10 AoA in Rectangular domain
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33Introduction to Venturi Scrubber
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34Blocking approach for ventrui scrubber
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35Blocking splits for major regions and deleting extra blocks
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36Blocking splits for throat and nozzles
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37Association, O-Grid for three nozzles, part mesh setup and premesh for approach
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38Second blocking approach for venturi scrubber
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45General discussion about the problem
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46Creating quarter O-Grid and adjusting blocking to geometry
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47Setting blocking with move vertices command
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48Deleting blocks (permanently) and merging vertices
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49Defining periodicity in blocking and association
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50Creating O-Grids for upper section and fine tuning of blocking
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51Final Association of edges to curves and vertices to points
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52Checking periodicity on vertices and faces and mesh export
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53Introduction
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54Creating half O-Grid and split for capturing geometry
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55Splitting and associating blocking at key locations
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56Deleting block permanently and fine tuning blocking
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57Further improvements in blocking
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58Splitting block for injection hole
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59Extrude block along curve for the injection hole
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60O-Grid for injection and final touches to mesh. Mesh check in Fluent
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