Academic Online Courses

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.

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

The problem numerically simulates one-step non-premixed hydrogen combustion with integration of the Sutherland viscosity and kinetic theory of thermal conductivity using ANSYS Fluent software. We design the 3-D model with the Spaceclaim software. We mesh the model with ANSYS Meshing software. The mesh type is Structured We use the Species Transport model to define a Combustion reaction. The combination of Sutherland viscosity and kinetic theory for thermal conductivity is presented for the accurate simulation of the combustion process. The standard k-e turbulence model is used to simulate the turbulence.

Price: $219

This study aims to investigate the aerodynamic performance of a Grumman RQ-4 Global Hawk using ANSYS Fluent. The Global Hawk geometry was modelled using SpaceClaim then imported into ANSYS Fluent for meshing consisting 3,764,695 elements. The simulation used a pressure-based solver.