Academic Online Courses

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.

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.

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: $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.

Price: $80

The study investigates Evaporation-Condensation Process in a Porous Heat Exchanger using ANSYS Fluent. The geometry is created in ANSYS Design Modeler, with a mesh of 8,777,268 elements generated using ANSYS Meshing. The simulation employs a pressure-based transient solver with the k-epsilon turbulence model and Volume of Fluid (VOF) multiphase model. It conducts a time-dependent analysis with enabled condensation in mass transfer mechanisms to simulate phase change from vapor to liquid water. Also, the domain is considered to be porous.

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.