CFD Intermediate Courses
Here's every CFD online course in the Intermediate level.
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
Quadcopter Fluid-Structure Interaction (FSI) Simulation using ANSYS Fluent
Intermediate, Advanced
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: $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.
Impact of Geometry on Heat Sink Performance
Beginner, Intermediate
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
Javelin Rocket Motion Simulation with Dynamic Mesh Method (Six DOF) using ANSYS Fluent
Intermediate, Advanced
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.
Cooling Clothing with Phase Change Material (PCM) Numerical Simulation
Beginner, Intermediate
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: $10
The problem numerically simulates the Fighter Helmet with Phase Change Material (PCM) using ANSYS Fluent The geometry is designed in SpaceClaim, and the meshing is performed using ANSYS Meshing. The mesh type is polyhedral, resulting in over 4 million elements. We aim to investigate the thermal performance and the effectiveness of incorporating Phase Change Material (PCM) for cooling.
Lockheed C-5 Galaxy Aerodynamic CFD Simulation
Beginner, Intermediate
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.
Combustion Processes in a Furnace CFD Analysis
Intermediate
Price: $16
This report details a Computational Fluid Dynamics (CFD) simulation of a furnace using ANSYS Fluent. The study investigates combustion processes, species transport, and NOx production to optimize furnace design and reduce emissions. The simulation employs a steady-state, pressure-based solver with the Realizable k-epsilon turbulence model. Results include density stratification, species distribution, temperature gradients, and flow patterns, providing valuable insights into combustion dynamics and pollutant formation within the furnace.