Mechanical Online Courses

Price: $32

This study extends the previous simulation of the VA-111 Shkval rocket using ANSYS Fluent software by incorporating mass transfer to capture the cavitation effects 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 To capture the cavitation effects, the Zwart-Gerber-BelAmri model is enabled

Price: $15

This study investigates the displacement of a net panel subjected to water flow using ANSYS Fluent simulation. The geometry of a square net panel was created using ANSYS Design Modeler. The computational domain was then discretized using ANSYS Meshing, resulting in over 2,339,853 elements. The simulation aims to analyze the net panel's fluid-structure interaction The structural model utilized a Linear Elasticity submodel to simulate the net panel’s deformation

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: $10

This problem simulates a Lockheed C-5 Galaxy using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using fluent Meshing with approximately 14 million cells. The simulation is carried out using the pressure-based solver. The turbulence model is set to Realizable k-ε.

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: $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: $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.