Industrial Online Courses

Price: $569

The problem numerically simulates a Radial Fuel Cell 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 2,393,706. We use the Fuel Cell and Electrolysis Model to define a fuel cell. We used the PEMFC sub-model to define a proton exchange membrane fuel cell. We used the Species model to define H2, O2, and H2O.

Price: $629

The problem numerically simulates the Electrolysis 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 2,393,706. We use the Fuel Cell and Electrolysis Model and the Electrolysis sub-model. We used the Species model to define H2, O2, and H2O.

Price: $499

In this project, we perform the numerical simulation of a PEM Fuel Cell Stack System using ANSYS Fluent software. We designed the geometry of the model in 3D using Design Modeler software. We meshed the model using ANSYS Meshing software, and 9,946,409 cells have been generated. We used the Fuel Cell and Electrolysis model and the PEMFC submodel to define the proton-exchange membrane fuel cell. We applied the Stack Management option to define multiple fuel cell units. The Species Transport model is automatically activated because of using the fuel cell model.

Price: $629

The problem numerically simulates Fuel Cell with Cooling System 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 4,984,882. We use the Fuel Cell and Electrolysis Model to define a fuel cell. We used the SOFC sub-model to define a solid oxide fuel cell. We used the Species model to define H2, O2, and H2O.

Price: $649

In this study, a comprehensive acoustic simulation of a quadcopter was performed using ANSYS Fluent Studying Acoustic, Pressure, and Motion analysis. 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 to define the rotational motion of the Quadcopter blades.

Price: Free

What are FSI and its appliance? 1-way FSI 2-way FSI

Price: Free

Appliances of CFD in flight dynamics Cmα derivative Cnβ derivative Clq derivative

Price: Free

Introduction to Aerodynamics and Aerospace Concepts in ANSYS Fluent Lift force and coefficient determination Drag force and coefficient determination Moment and moment coefficient determination Types of shock wave and shock wave determination

Price: $649

The problem numerically simulates the dynamic stability derivatives of a flying wing aircraft using ANSYS Fluent The Mesh Motion and UDF files are used to define the rotational and oscillatory motion of the wing. The 3D geometry of the model was created using ANSYS SpaceClaim A high-quality unstructured mesh was generated using ANSYS Meshing The corresponding graphs are drawn and the total number of 24 dynamic derivatives coefficients are correctly extracted.