MR CFD’s All Courses
Here's every Course from Basic to Advanced, that can boost your skills and career.
Fluidized Bed Bio-Reactor ANSYS Fluent Training
Intermediate, Advanced
Price: $64
The problem numerically simulates the fluidized bed bio-reactor using ANSYS Fluent software. The geometry is designed in a 2D model with the ANSYS Design Modeler software. We performed the structured mesh of the model with ANSYS Meshing software, and the element number equals 26,289. The Eulerian model was used to simulate the multiphase behavior of the solution. The project is solved in transient state.
Sub-Oceanic Volcanic Activity ANSYS Fluent Training
Intermediate, Advanced
Price: $36
The problem numerically simulates the Sub-Oceanic Volcanic Activity using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We mesh the model with ANSYS Meshing software, and the element number equals 42,751. We perform this simulation as unsteady (Transient). The multiphase VOF model is used to model the three phases of air, water and vapor. Evaporation and condensation is used for mass transfer mechanism.
Price: $24
The problem numerically simulates the Microfluidic Droplet Generator using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We mesh the model with ANSYS Meshing software, and the element number equals 10,441. We perform this simulation as unsteady (Transient). The multiphase VOF model is used to model the phases of water and oil. Surface tension modeling along wall adhesion is enabled.
Boat Propeller, Steady State ANSYS CFX Training
Beginner, Intermediate, Advanced
Price: $100
The problem numerically simulates the rotation of Boat Propeller using ANSYS CFX software. The geometry is designed in a 3D model with the SpaceClaim software. We performed the mesh of the model with ANSYS Meshing software, and the element number equals 4,037,941. Frozen Rotor is set for frame change model of the interfaces.
Contra-Rotating Turbine CFD Simulation Training
Intermediate
Price: $42
In this project, a flow around a Contra-Rotating Turbine has been simulated, and the results of this simulation have been investigated. This ANSYS Fluent CFD training simulates a contra-rotating VAWT turbine with two blade rows rotating oppositely at 14.7 rad/s. Inlet velocity is 5.3 m/s; mesh motion defines rotations using k-epsilon model and steady pressure-based solver. Results show enhanced pressure/velocity between blades, doubling torque (~1.9 N.m per row) for better power.
Fluid-Structure Interaction over HAWT Turbine Vibration (one-way)
Intermediate, Advanced
Price: $54
The problem numerically simulates the Fluid-Structure Interaction over HAWT Turbine using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. Mesh grid is generated using ANSYS Meshing , and the element number equals 3,465,821. The MRF method is used to rotate the turbine. FSI model analyses total strain, and stress over the turbine.
Porous Zone Inside 3D Channel ANSYS CFX Tutorial
Beginner, Intermediate, Advanced
Price: $60
The problem numerically simulates a Porous Zone inside 3D cylinder using ANSYS CFX software. We modeled the geometry using ANSYS Design Modeler and created the mesh using ANSYS Meshing software. The mesh type is Structured and the number of them is 1,308,762. Porosity has been used in the simulation. Pressure Drop inside the channel due to porosity is investigated.
Von Kármán Effect over Cylinder, ANSYS CFX
Beginner, Intermediate, Advanced
Price: $80
The problem numerically simulates the Von Kármán effect behind a cylinder using ANSYS CFX software. The geometry is designed in a 2.5D model with the Design Modeler software. We performed the mesh of the model with ANSYS Meshing software, and the element number equals 77,262. Body of Influence option is used to create smaller elements around the cylinder. The Transient and Steady form of the solution is performed.
Price: $649
The problem numerically simulates the dynamic stability derivatives of a flying wing aircraft using ANSYS Fluent The Mesh Motion and UDF files are used to define the rotational and oscillatory motion of the wing. The 3D geometry of the model was created using ANSYS SpaceClaim A high-quality unstructured mesh was generated using ANSYS Meshing The corresponding graphs are drawn and the total number of 24 dynamic derivatives coefficients are correctly extracted.