CFD Intermediate Courses

Price: $80

The study investigates Evaporation-Condensation Process in a Porous Heat Exchanger using ANSYS Fluent. The geometry is created in ANSYS Design Modeler, with a mesh of 8,777,268 elements generated using ANSYS Meshing. The simulation employs a pressure-based transient solver with the k-epsilon turbulence model and Volume of Fluid (VOF) multiphase model. It conducts a time-dependent analysis with enabled condensation in mass transfer mechanisms to simulate phase change from vapor to liquid water. Also, the domain is considered to be porous.

Price: $14

The study investigates cavitation in water flow around a triangular obstacle using ANSYS Fluent CFD simulation. The geometry is created in ANSYS Design Modeler, with a mesh of 310,000 structured elements generated using ANSYS Meshing. The simulation employs a pressure-based transient solver with the k-epsilon turbulence model and Volume of Fluid (VOF) multiphase model. ANSYS Fluent conducts a time-dependent analysis with enabled cavitation in mass transfer mechanisms to simulate phase change from liquid water to vapor.

Price: $48

This study simulates diesel-air mixture flow with fuel droplet evaporation using ANSYS Fluent CFD software. The 3D cylindrical chamber geometry is designed in SpaceClaim. Meshing is performed using ANSYS Meshing, resulting in over 2 million elements. The Species Transport model with Eddy-Dissipation is employed for turbulence-chemistry interaction. The Discrete Phase Model (DPM) is utilized to simulate fuel droplet movement and evaporation.

Price: $30

The problem numerically simulates the Fluid-Structure Interaction over Vertical Turbine using ANSYS Fluent software. We designed the 3-D model using the Design Modeler software. The mesh grid is generated using ANSYS Meshing, and the element number equals 705,465. The Frame Motion method is used to rotate the turbine. FSI model analyses total strain, and stress over the VAWT turbine.

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: $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.