Aerodynamics & Aerospace Online Courses

Here's every CFD online course related to Aerodynamics & Aerospace category.

168 Courses

Price: $36

The problem numerically simulates Shock waves in a Supersonic Airflow using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software, and the element number equals 4466857. We perform this simulation as unsteady (Transient). We use the Density-Based solver to define the compressible flow.

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This project is going to simulate an airfoil in the airflow field with a 16-degree attack angle.

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Price: $20

The problem numerically simulates NACA 0012 Airfoil (Compressible Flow) using ANSYS Fluent software. We design the 2-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing. The model mesh is structured, and 35000 cells have been created. We apply a Density-based solver to define the compressible flow. We determine the Mach number for the inlet boundary condition.

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The problem numerically simulates Airflow on the Dimpled Rotating Cylinder 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 1064903. We use the Frame Motion method to define the rotational movement.

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Price: $36

The problem numerically simulates Magnetic Force Effect on NACA 0015 airfoil using ANSYS Fluent software. We design the 3-D model by the Design Modeler software. We Mesh the model by ANSYS Meshing software. We use the MHD model to consider the magnetic force effect on the flow.

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Price: $28

The present study investigates the airflow passing over a 3-blade horizontal axis wind turbine (HAWT) by ANSYS Fluent software. The present 3-D model was designed by SOLIDWORKS software and imported to Design Modeler software. The meshing of the model has been done using ANSYS Meshing software. The mesh type is structured, and the element number is 4270222. The present simulation aims to investigate the effect of wind flow on the turbine blades and calculate the Drag and Lift forces applied to the blade surfaces. Using the Frame Motion (MRF) method.

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