Industrial Online Courses

Price: $249

This product numerically simulates the Pouch Battery Discharge 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 125401. We use the MSMD (Multi-Scale Multi-Domain) Battery model to define the charge/discharge. We use Newman's P2D (Pseudo 2-D) sub-model to determine the electrochemical computations. The run calculation is in an unsteady state (transient).

Price: $249

This product numerically simulates the Pouch Battery Discharge 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 13601. We use the MSMD (Multi-Scale Multi-Domain) Battery model to define the charge/discharge. We use the ECM (Equivalent Circuit Model) sub-model to determine the electrochemical computations. The run calculation is in an unsteady state (transient).

Price: $249

This product numerically simulates the Pouch Battery Discharge using ANSYS Fluent software. We design the 3-D model with Design Modeler software. We mesh the model with ANSYS Meshing software. The mesh is Structured, and the element number equals 1210. We use the MSMD (Multi-Scale Multi-Domain) Battery model to define the charge/discharge. We use the NTGK sub-model to determine the electrochemical computations. The run calculation is in an unsteady state (transient).

Price: $319

Taxi Drone Ansys Fluent Simulation involves using advanced CFD software to analyze the aerodynamic performance of urban air mobility vehicles The geometry of the taxi drone was designed using ANSYS SpaceClaim , The mesh was generated using ANSYS Meshing, resulting in a total of 2,829,977 elements The velocity inlet was set to 30 m/s with an angle of attack of 5 degrees. The rotational speed of the blades was configured with MRF method at 5000 RPM, with the upper and lower blades rotating in opposite directions.

Price: $319

This study focuses on the aerodynamic analysis of the Switchblade 300 using ANSYS Fluent Two scenarios are simulated: one with the rear blade stationary and the other with the rear blade in motion. The geometry of the Switchblade was created using SpaceClaim software,The meshing was performed in Fluent Meshing, utilizing a polyhedral mesh with over 7,600,000 elements The Multiple Reference Frame (MRF) approach was employed to simulate the rotating rear blade at 5000 RPM.

Price: $24

This study uses CFD simulation to investigate the water tank filling process The geometry of the tank was created using ANSYS Design Modeler, and the computational domain was discretized using ANSYS Meshing, resulting in over 135,000 elements The Volume of Fluid (VOF) model was employed to simulate the interaction between water and air phases A User-Defined Function (UDF) was implemented to control the time step size

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: $649

This study presents a Fluid-Structure Interaction (FSI) simulation of a quadcopter using ANSYS Fluent The quadcopter geometry was created using ANSYS SpaceClaim The model was then meshed using ANSYS Meshing, which generated an unstructured mesh consisting of approximately 499,152 elements To accurately capture the blades’ rotation, two frame motion(MRF) zones are applied to the blades. The Structure model with the Linear Elasticity option was enabled to investigate the displacement of the blade

Price: $949

This project numerically simulates the PEM 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 Structured mesh including 270,0000 elements is generated. We use the Fuel Cell and Electrolysis Model to define a fuel cell system. 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. The present CFD work is Validated with a reference Article.