Fluent Meshing Online Courses

Price: Free

Master ANSYS Fluent Meshing with this comprehensive course covering advanced techniques for creating high-quality meshes for complex CFD simulations. Learn structured and unstructured meshing methods, boundary layer refinement, mesh quality improvement, and workflow optimization through practical examples.

Price: $319

This study focuses on the aerodynamic analysis of the Switchblade 300 using ANSYS Fluent Two scenarios are simulated: one with the rear blade stationary and the other with the rear blade in motion. The geometry of the Switchblade was created using SpaceClaim software,The meshing was performed in Fluent Meshing, utilizing a polyhedral mesh with over 7,600,000 elements The Multiple Reference Frame (MRF) approach was employed to simulate the rotating rear blade at 5000 RPM.

Price: $31.50

The problem numerically simulates the Lockheed Martin F-22 Raptor using ANSYS Fluent The geometry is designed in SpaceClaim, and the meshing is performed using fluent Meshing. The mesh type is polyhedral, and the element number equals 4,989,000. We aim to Maximize the Lift-to-Drag Ratio of wings. We use the Adjoint Solver to analyze the Shape Sensitivity. The Design Optimization is performed with the Gradient-based Radial Basis Function (RBF) used to apply Mesh Morphing.

Price: $14

This problem simulates a VA-111 Shkval rocket using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using Fluent Meshing; the element number equals 257,000 polyhedral cells. The simulation uses the Pressure-based and VOF Multiphase model to define a two-phase flow. The turbulence model is set to SST k-ω.

Price: $225

The problem numerically simulates the Northrop Grumman RQ-4 Global Hawk using ANSYS Fluent The geometry is designed in SpaceClaim, and the meshing is performed using fluent Meshing. The mesh type is polyhedral, and the element number equals 2,063,629. We aim to Maximize the Lift-to-Drag Ratio of wings. We use the Adjoint Solver to analyze the Shape Sensitivity. The Design Optimization is performed with the Gradient-based The Radial Basis Function (RBF) is used to apply Mesh Morphing.

Price: $30

This problem simulates a F-22 aircraft using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using FLUENT Meshing. The simulation is carried out using the density-based solver. The turbulence model is set to k-ε Realizable.

Price: $8

This product simulates a shell and plate heat exchanger using ANSYS Fluent software. The geometry of the problem is designed in spaceclaim. Then the Fluent meshing software was used to mesh the geometry producing 3,686,338 polyhedral elements. The turbulence of the flow is simulated via Realizable k-e model.

Price: $28

In this project, the combustion of methane in a gas stove was modeled using ANSYS Fluent. Methane mechanism was chosen for reaction mechanism and eddy dissipation model used for turbulence-chemistry. The geometry was created in Design Modeler, and a mesh consisting of 5,533,297 elements was generated using Fluent Meshing.

Price: $30

This project numerically simulates the Vortex Tube using ANSYS Fluent software. The 3-D geometry is designed in Space Claim software. We used Fluent Meshing Software to generate mesh; the element number equals 497,635. Turbulent flow is modeled with the Spalart Almaras model. The solver is Density-Based and the Sutherland model is used for viscosity.