ANSYS Fluent Online Courses

Price: $489

The problem numerically simulates the Fluid-Structure Interaction over Northrop Grumman RQ-4 Global Hawk using ANSYS Fluent software. The Global Hawk geometry was modeled using SpaceClaim and then imported into ANSYS meshing for meshing consisting of 5,056,067 non-conformal elements. The simulation used a pressure-based solver. One way FSI model analyses total strain, and stress over the turbine.

Price: $30

The study conducts a CFD analysis of sand particle sedimentation using ANSYS Fluent software. We design the cylindrical geometry using ANSYS Design Modeler. We mesh the model using ANSYS Meshing software, resulting in 388,797 hexahedral elements. We use the Eulerian multiphase model to simulate three different sizes of sand particles (small, medium, and large) interacting with the fluid phase. We aim to predict the sedimentation patterns and particle distribution for different sand sizes, analyzing density, pressure, and volume fraction contours.

Price: $36

In this project, a V-Flame is simulated using the Zimont model, then compared with the paper "Numerical simulation of a premixed turbulent V-shaped flame." by Ansys Fluent software. Premixed combustion of methane-air is ​​simulated, comparing the Zimont and Eddy Break-Up models. The geometry is designed in Spaceclaim software. A structured grid is used to create a mesh in the computing domain using ANSYS Meshing software.

Price: $12

This study presents a CFD simulation of multi-fuel combustion in a combustion chamber using ANSYS Fluent. The 3D geometry was designed in SpaceClaim and meshed in ANSYS Meshing with over 3.6 million polyhedra elements. The simulation employs the Species Transport Model with the Eddy-Dissipation model for turbulence-chemistry interaction. The analysis effectively captures key combustion dynamics, including temperature distribution, species mass fractions, flow patterns, and turbulence flame speed within the chamber.

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: $140

This study presents a CFD analysis of methane-air combustion in a gas turbine combustor using ANSYS Fluent. The 3D geometry represents a quarter section of a cylindrical combustor, designed in ANSYS SpaceClaim. ANSYS Meshing is used to generate a high-resolution mesh with over 2 million elements. The simulation employs the Species Transport model with Volumetric Reaction and the Eddy-Dissipation model for turbulence-chemistry interaction. The analysis effectively captures key combustion dynamics, including species distribution, temperature profiles, pressure variations, and velocity fields within the combustor.

Price: $15

This project simulates the Fluid-Structure Interaction (FSI) of a high-speed airfoil using ANSYS Fluent software. The airfoil geometry is designed in ANSYS Design Modeler. ANSYS Meshing is used to generate a high-quality mesh with 2,398,833 elements. In this study, the complex flow behavior and structural response of the airfoil are simulated using a pressure-based transient solver and the Realizable k-epsilon turbulence model. The pressure distribution, velocity patterns, and airfoil displacement under high-speed conditions are well modeled in this project.

Price: $100

This problem simulates Adhesion effect on a self-cleaning material (porous)using Ansys Fluent software. The 2-D geometry is designed in Design Modeler software. Ansys Meshing software is used to generate the mesh; the element number equals 105,000. In this project, the Hydrophilicity and hydrophobicity of surfaces is simulated using the VOF How the flow pattern near a hydrophobic surface and near a hydrophobic surface is well modeled in this project.

Price: $4

This report presents a comprehensive CFD analysis of a Gas Turbine Intake using ANSYS Fluent. The study investigates flow behavior and pressure characteristics within a complex intake geometry, utilizing a structured mesh of 1,494,720 elements. The simulation employs a pressure-based, steady-state solver with the Realizable k-epsilon turbulence model. Key results include velocity magnitude contours, pressure distribution, and turbulence kinetic energy patterns throughout the intake system. An area-weighted average pressure of 320.84187 Pa at the inlet offers quantitative data on entrance conditions.