Aerodynamics & Aerospace Online Courses

Price: $219

The problem numerically simulates a ScanEagle UAV using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with ANSYS Meshing software. The element number equals 3,213,450 and their type is polyhedra. Multiple Reference Frames (Frame Motion) are used to model the rotational motion of the propeller.

Price: $219

The problem numerically simulates a VTOL UAV using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with Fluent Meshing software. The element number equals 1,761,160 and their type is polyhedra. Multiple Reference Frames (MRF) are used to model the rotational motion of propellers.

Price: $30

The problem numerically simulates the Supersonic Jet Ramped Intake 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 element number equals 1278343. We have used the density-based solver due to the compressibility.

Price: $10

The problem numerically simulates the High-Bypass Turbofan Engine using ANSYS Fluent software. We design the 3-D model with the Design Modeler software. We mesh the model with ANSYS Meshing software. The element number equals 16,635,982. The MRF method (Frame Motion) is used to define fan rotation.

Price: $32

The problem numerically simulates the Darrieus Wind Turbine motion using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. We mesh the model with ANSYS Meshing software. The element number equals 2,966,928. We use the 6DOF Dynamic Mesh method to define the turbine rotation. Remeshing and Smoothing mesh methods are also used.

Price: $225

The problem numerically simulates the drag force on a simple cylindrical obstacle using ANSYS Fluent software. We design the 2-D model by the Design Modeler software and then mesh it with ANSYS Meshing software. The mesh type is Structured, and the element number equals 36000. We aim to Minimize the drag force in a three-step simulation. We use the Adjoint Solver to analyze the Shape Sensitivity. The Design Optimization is performed with the Gradient-based Optimizer. We use the Radial Basis Function (RBF) to apply Mesh Morphing.

Price: $225

The problem numerically simulates lift to drag ratio on an airfoil using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We mesh the model with ANSYS Meshing software, and the element number equals 207521. We aim to Maximize the lift to drag ratio in a three-step simulation. We use the Adjoint Solver to analyze the Shape Sensitivity. The Design Optimization is performed with the Gradient-based Optimizer. We use the Radial Basis Function (RBF) to apply Mesh Morphing.

Price: $42

The problem numerically simulates the Vertical Axis Wind Turbine (VAWT) using ANSYS Fluent software. We design the 3-D model by the Design Modeler and create the mesh using ANSYS Meshing software. The element type is Hybrid (Structured and Unstructured) and their number equals 904,145. The Mesh Motion option is enabled to define the rotational motion of the wind turbine.

Price: $140

The problem numerically simulates the Horizontal Axis Wind Turbine (HAWT) using ANSYS Fluent software. We design the 3-D model by the Design Modeler and create the mesh using ANSYS Meshing software. The element number equals 2,696,011. The MRF option (Frame Motion) is enabled to define the rotational motion of the wind turbine.