MR CFD’s All Courses

Price: $12

This report details a nanoparticle simulation conducted using ANSYS Fluent The simulation geometry consists of a rectangular cuboid created in SpaceClaim . Meshing was performed in ANSYS Meshing, resulting in a grid of 151,294 triangular cells Discrete Phase Model (DPM) activated, Flow and turbulence equations deactivated

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: $949

This project numerically simulates the PEM Fuel Cell using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with ANSYS Meshing software and the Structured mesh including 270,0000 elements is generated. We use the Fuel Cell and Electrolysis Model to define a fuel cell system. We used the PEMFC sub-model to define a proton-exchange membrane fuel cell. We used the Species model to define H2, O2, and H2O. The present CFD work is Validated with a reference Article.

Price: $12

This study presents a CFD analysis of a Multi-point Liquid Distributor for packed columns using ANSYS Fluent. We designed the 3-D symmetry model using the ANSYS Design Modeler We mesh the model with ANSYS Meshing software, and the element number equals 783,039. The Volume of Fluid (VOF) model was utilized to simulate the multiphase flow of water and air. A steady-state, pressure-based solver was employed for the simulation.

Price: $14

This study compares the thermal performance of open and enclosed heat sink designs using CFD simulations The open design features exposed fins, while the enclosed design has a closed-top 3-D symmetry model designed using ANSYS Design Modeler software model meshed with ANSYS Meshing software, and the element number equals 2,599,334. The discrete Ordinates (DO) radiation model was activated to simulate the impact of solar irradiation

Price: $8

This study investigates the thermal and fluid dynamics behavior of a pin-fin heat exchanger using CFD simulation. The geometry of the pin-fin heat exchanger was created using ANSYS Design Modeler. The computational domain was then discretized using ANSYS Meshing, resulting in 1,679,530 elements. The pin wall temperature was set to a constant 800 K to simulate a high-temperature heat source

Price: $429

This report presents a simulation of the motion of a javelin rocket using the dynamic mesh method The geometry of the javelin rocket is created using Spaceclaim software A high-quality mesh is generated around the rocket geometry using ANSYS Meshing(about 250,000 elements) The six DOF solver settings are specified, including the mass properties and the degrees of freedom for translation and rotation.

Price: $8

numerical simulation study of cooling clothing designed to regulate body temperature using ANSYS Fluent The geometry is designed in SpaceClaim, and the meshing is performed using Ansys Meshing. The mesh type is triangular, resulting in a mesh with approximately 5 million elements. We aim to investigates the effectiveness of incorporating Phase Change Material (PCM) into the clothing.. Two simulations were conducted: one without PCM and another with PCM incorporated into the clothing

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.