Academic Online Courses

Price: $649

The problem numerically simulates the Dynamic Stability Derivatives of the Javelin Rocket using ANSYS Fluent. We designed the 3-D model using the SpaceClaim. We mesh the model with ANSYS Meshing software, and the element number equals 4,245,614. We perform this simulation as unsteady (Transient). We use the Mesh Motion and UDF files to define the rotational and oscillation motion of the Rocket.

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: $360

The study conducts a CFD analysis of aortic valve displacement using ANSYS Workbench. The geometry is designed in SpaceClaim based on CT-scan data, with a mesh of 67,926 fluid elements and 627,914 solid elements. The simulation uses a pressure-based transient solver with a laminar flow model. System coupling between Transient Structural and Fluent enables analysis of valve leaflet movement and blood flow interaction. Results show pressure gradients, velocity patterns, wall shear stress distribution, and valve leaflet deformation.

Price: $319

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

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: $45

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.