
Ansys software download link
https://www.ansys.com/en-in/academic/free-student-products
Model an axial compressor rotor grid in turbogrid using rotor 37 coordinates, including hub, blade, and shroud profiles with six airfoil coordinates in cartesian coordinates.
Import blade coordinates into Turbogrid, switch units to millimeters, set machine data for 36 blades on the x axis, import hub, shroud, and blade profiles, and save state rotor37.
Edit the blade mesh to reduce errors by adjusting maximum and minimum face angles, insert a spanwise layer, and save as rotor_37.gtm for CFX or fluent.
Create and edit the axial turbine blade mesh by setting target passage mesh size, boundary layer y+, and spanwise distribution, then export the final .gtm mesh for CFD.
Use Ansys TurboGrid to build inlet, blade, and outlet domains; adjust hub and shroud with parametric and points methods, then refine boundary layer to reach target y+.
Refine an axial compressor mesh in Ansys TurboGrid by importing blade coordinates, setting shroud tip clearance, extending inlets and outlets, adjusting boundary layer y+, and exporting the final mesh.
Mesh a centrifugal compressor blade in Turbogrid by importing hub, shroud, and profile data for a 20-blade lscc, set tip clearance, and refine boundary layer with y+ and spanwise elements.
Model a centrifugal compressor with splitter blades in turbo grid by importing .tse session and profile files, setting tip clearance, boundary conditions, and refining the mesh with edge split controls.
Mesh a vane diffuser for a NASA lowspeed centrifugal compressor using turbogrid, modeling a single periodic sector.
Model and mesh a centrifugal compressor in turbogrid for assignment by importing profile curves, configuring blade count, axis of rotation, coordinates, and tip clearance, and visualizing hub and shroud profiles.
Open turbo grid launcher, import 14-blade impeller for a centrifugal compressor, set 1 mm tip clearance, apply boundary layer y+ and Reynolds 1e6, export mesh state and gtm for cfd.
This course provides the complete fundamentals of Ansys Turbogrid meshing for turbomachinery components.
The course contents include demonstration of mesh generation for axial compressors, centrifugal compressors and axial turbines. This course provides basics of TurboGrid, details on how to input blade data, advanced mesh generation techniques and error handling methods. There are two NASA test cases included in the course. The mesh generated for these models can be used for CFD validation purpose.
Two assignments are provided in this course for practicing mesh generation using turbogrid. This will help to get hands on experience with the software. The detailed modules cover everything from axial compressor rotor meshing to centrifugal compressor with splitter blade meshing and vaned diffuser meshing. With practical assignments, you'll reinforce your learning and be ready to handle real-world problems
There is a bonus part in the end, which demonstrates how to import the generated mesh into Ansys CFX, solve and post-process the results. This is to provide basic understanding of the operation of gas turbine components.
Further, in the bonus section, demo is given on how to import cad model into Ansys Blademodeler and export it to turbogrid input format. By this way, you can create mesh in turbogrid for cad input files.