SpaceClaim Online Courses

Price: $319

This problem simulates a javelin rocket using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using ANSYS Meshing. The simulation is carried out using the density-based solver. The turbulence model is set to Realizable k-ε.

Price: $48

This study simulates diesel-air mixture flow with fuel droplet evaporation using ANSYS Fluent CFD software. The 3D cylindrical chamber geometry is designed in SpaceClaim. Meshing is performed using ANSYS Meshing, resulting in over 2 million elements. The Species Transport model with Eddy-Dissipation is employed for turbulence-chemistry interaction. The Discrete Phase Model (DPM) is utilized to simulate fuel droplet movement and evaporation.

Price: $489

The problem numerically simulates the Fluid-Structure Interaction over Northrop Grumman RQ-4 Global Hawk using ANSYS Fluent software. The Global Hawk geometry was modeled using SpaceClaim and then imported into ANSYS meshing for meshing consisting of 5,056,067 non-conformal elements. The simulation used a pressure-based solver. One way FSI model analyses total strain, and stress over the turbine.

Price: $12

This study presents a CFD simulation of multi-fuel combustion in a combustion chamber using ANSYS Fluent. The 3D geometry was designed in SpaceClaim and meshed in ANSYS Meshing with over 3.6 million polyhedra elements. The simulation employs the Species Transport Model with the Eddy-Dissipation model for turbulence-chemistry interaction. The analysis effectively captures key combustion dynamics, including temperature distribution, species mass fractions, flow patterns, and turbulence flame speed within the chamber.

Price: $30

This problem simulates a F-22 aircraft using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using FLUENT Meshing. The simulation is carried out using the density-based solver. The turbulence model is set to k-ε Realizable.

Price: $140

This study presents a CFD analysis of methane-air combustion in a gas turbine combustor using ANSYS Fluent. The 3D geometry represents a quarter section of a cylindrical combustor, designed in ANSYS SpaceClaim. ANSYS Meshing is used to generate a high-resolution mesh with over 2 million elements. The simulation employs the Species Transport model with Volumetric Reaction and the Eddy-Dissipation model for turbulence-chemistry interaction. The analysis effectively captures key combustion dynamics, including species distribution, temperature profiles, pressure variations, and velocity fields within the combustor.

Price: $8

This product simulates a shell and plate heat exchanger using ANSYS Fluent software. The geometry of the problem is designed in spaceclaim. Then the Fluent meshing software was used to mesh the geometry producing 3,686,338 polyhedral elements. The turbulence of the flow is simulated via Realizable k-e model.

Price: $219

This study aims to investigate the aerodynamic performance of a Grumman RQ-4 Global Hawk using ANSYS Fluent. The Global Hawk geometry was modelled using SpaceClaim then imported into ANSYS Fluent for meshing consisting 3,764,695 elements. The simulation used a pressure-based solver.

Price: $18

This project aims to evaluate the impact of tube geometry and nanofluid composition on heat transfer performance. Three nanofluid compositions are examined: Alumina/water, MWCNT/water, and a hybrid Alumina-MWCNT/water nanofluid. It explores two geometric configurations: circular and diamond-shaped tubes' effect on heat transfer performance. The turbulence of the flow is simulated by Realizable k-epsilon model. The single phase model is considered to simulate nanoparticle presence in the base fluid.