Moving Reference Frame (MRF) Online Courses

Price: $319

This study focuses on the aerodynamic analysis of the Switchblade 300 using ANSYS Fluent Two scenarios are simulated: one with the rear blade stationary and the other with the rear blade in motion. The geometry of the Switchblade was created using SpaceClaim software,The meshing was performed in Fluent Meshing, utilizing a polyhedral mesh with over 7,600,000 elements The Multiple Reference Frame (MRF) approach was employed to simulate the rotating rear blade at 5000 RPM.

Price: $649

The problem numerically simulates the Dynamic Stability Derivatives of Quadcopter using ANSYS Fluent We designed the 3-D symmetry model using the SpaceClaim We mesh the model with ANSYS Meshing software, and the element number equals 1,710,236. We perform this simulation as unsteady (Transient). We use the Mesh Motion and UDF files to define the rotational and oscillation motion of the Quadcopter and blades.

Price: $649

This study presents a Fluid-Structure Interaction (FSI) simulation of a quadcopter using ANSYS Fluent The quadcopter geometry was created using ANSYS SpaceClaim The model was then meshed using ANSYS Meshing, which generated an unstructured mesh consisting of approximately 499,152 elements To accurately capture the blades’ rotation, two frame motion(MRF) zones are applied to the blades. The Structure model with the Linear Elasticity option was enabled to investigate the displacement of the blade

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: $56

This study investigates the flow dynamics in a steam turbine using CFD analysis in ANSYS Fluent. The 3D geometry was created in SpaceClaim and meshed using ANSYS Meshing, resulting in about 19 million tetrahedral elements. The simulation utilizes the Realizable k-ε turbulence model with standard wall function and includes the energy equation for temperature analysis. A density-based solver with real-gas-peng-robinson model is employed for compressible flow.

Price: $64

This project investigates turbocharger performance using CFD analysis in ANSYS Fluent, focusing on the fluid flow and thermal behavior of air through a one-sixth periodic sector of the geometry. The geometry was prepared using Vista CCD and BladeGen, and the mesh was generated with TurboGrid as a structured grid containing 972,176 cells. A pressure-based solver with the SST k-ω, k-ω turbulence model was used, and blade rotation was simulated at 92,000 RPM with the Frame Motion approach. The results highlight the influence of geometry on flow patterns, pressure distribution, and temperature gradients, offering insight into compression efficiency and overall turbocharger performance.

Price: $16

The present problem simulates a Six Blade Stirring Mixer using ANSYS Fluent software. We have designed the geometry using DesignModeler software and created the mesh on this geometry using ANSYS Meshing software. The mesh type is unstructured with 5,447,852 cells. The Mixture multiphase model has been used to simulate the present model. The Multiple Reference Frames (MRF) model is used to simulate the motion of impeller. The solution is steady, and the k-Ꜫ model is chosen to simulate the turbulence of the flow.

Price: $32

The current CFD Analysis numerically Validates the Paper "Experimental study of shrouded micro-wind turbine" via ANSYS Fluent software. We have designed and meshed the geometry using Design Modeler and ANSYS Meshing then meshing in fluent, producing 2,356,897 polyhedral elements. MRF is used to simulate rotating zone. The turbulence of the flow is simulated via K-w sst model.

Price: $320

The current CFD Analysis numerically validates the Paper "CFD Investigation on the aerodynamic characteristics of a small-sized wind turbine of NREL PHASE VI operating with a stall-regulated method" via ANSYS Fluent software. We have designed and meshed the geometry using Spaceclaim and ANSYS Meshing then meshing in fluent, producing 5,466,728 elements. MRF is used to simulate rotating zone. The turbulence of the flow is simulated via Realizable k-epsilon model.