SpaceClaim Online Courses

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: $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: $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.

Price: $14

This problem simulates a VA-111 Shkval rocket using ANSYS Fluent software. The geometry is designed in SpaceClaim, and the meshing is performed using Fluent Meshing; the element number equals 257,000 polyhedral cells. The simulation uses the Pressure-based and VOF Multiphase model to define a two-phase flow. The turbulence model is set to SST k-ω.

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.

Price: $225

The problem numerically simulates the Northrop Grumman RQ-4 Global Hawk 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 2,063,629. 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 The Radial Basis Function (RBF) is used to apply Mesh Morphing.

Price: $649

The problem numerically simulates the Dynamic Stability Derivatives of the Javelin Rocket using ANSYS Fluent. We designed the 3-D model using the SpaceClaim. We mesh the model with ANSYS Meshing software, and the element number equals 4,245,614. We perform this simulation as unsteady (Transient). We use the Mesh Motion and UDF files to define the rotational and oscillation motion of the Rocket.

Price: $360

The study conducts a CFD analysis of aortic valve displacement using ANSYS Workbench. The geometry is designed in SpaceClaim based on CT-scan data, with a mesh of 67,926 fluid elements and 627,914 solid elements. The simulation uses a pressure-based transient solver with a laminar flow model. System coupling between Transient Structural and Fluent enables analysis of valve leaflet movement and blood flow interaction. Results show pressure gradients, velocity patterns, wall shear stress distribution, and valve leaflet deformation.