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This training package includes 10 practical aerodynamic and aerospace engineering exercises using ANSYS Fluent software. MR CFD suggests this package for all aerodynamic and aerospace engineers who will learn CFD simulation in this field at the ADVANCED level.

#### Icing of a 3-D Airfoil Surface CFD Simulation, ANSYS Fluent Tutorial

• The problem numerically simulates the Icing of a 3-D Airfoil Surface 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 978532.
• We perform this simulation as unsteady (Transient).
• We use the Eulerian Wall Film (EWF) model to estimate the formation of a thin film of liquid on the wall surfaces.

#### Impeller of an Electrical Motor, Airflow Analysis

• The problem numerically simulates the Impeller of an Electrical Motor 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 1786708.
• We use the Frame Motion method to define the rotation of the impeller.

#### Compressible Flow around an Aerial Structure by LES

• The problem numerically simulates the compressible flow around an aerial structure 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 5515041.
• We perform this simulation as unsteady (Transient).
• We use the Density-based solver to define the compressible flow.

#### Stall Investigation Over a Wing, ANSYS Fluent CFD Simulation Training

• The problem numerically simulates the Stall phenomenon over a Wing using ANSYS Fluent software.
• We design the 3-D model by the Design Modeler software.
• We Mesh the model by ANSYS Meshing software.
• The air is assumed to be incompressible.

#### Acoustic CFD Simulation (LES) of airflow over Cylinders in 4 Different Positions, Ansys Fluent Training

• The problem numerically simulates the Acoustic airflow over Cylinders in Different Positions (LES) using ANSYS Fluent software.
• We Mesh the model by ANSYS Meshing software.
• The mesh type is Structured, and the element number equals 2000000.
• We perform this simulation as unsteady (Transient).
• We use the Ffowcs-Williams & Hawking’s equations to model Acoustic in the present work.

#### Inviscid Supersonic Flow Over F-16 Aircraft Simulation

In this project, Inviscid Supersonic Flow Over F-16 Aircraft has been simulated, and the results of this simulation have been investigated.

#### Magnetic Force Effect on an Airfoil CFD Simulation, ANSYS Fluent Tutorial

• 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.

#### NACA0012 Airfoil, Compressible Flow, Paper Validation

In this project, we intend to simulate the NACA0012 airfoil with the compressible flow around it to compare and validate the results with the results in the article.

#### FSI Analysis of Airflow around an Airfoil Vibration

• The problem numerically simulates the airflow around an airfoil using ANSYS Fluent software.
• This project is performed by the fluid-structure interaction (FSI) method.
• We design the 2-D model with the Design Modeler software.
• We Mesh the model with ANSYS Meshing software, and the element number equals 56220.
• We perform this simulation as unsteady (Transient).
• We use the Dynamic Mesh method to consider grid changes over time.
• We apply the System Coupling to communicate between Fluent and Transient Structural software.
• We use the Density-based solver to consider compressible flow.
• We use a UDF to determine variable velocity and attack angle.

#### Acoustic in a Turbojet Intake Fan CFD Simulation

• The problem numerically simulates Acoustic in a Turbojet (Intake Fan) 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 3723166.
• We use the Density-based solver to consider compressible flow.
• We use the Frame Motion (MRF) to define the rotational movement.
• We use the Broadband Noise Sources model to define the Acoustic model.

## Aerodynamic & Aerospace ANSYS Fluent CFD Simulation Training Package for ADVANCED Users (10 Projects)

This training package includes 10 practical aerodynamic and aerospace engineering exercises using ANSYS Fluent software. MR CFD suggests this package for all aerodynamic and aerospace engineers who will learn CFD simulation in this field at the ADVANCED level.

### Icing

Practical exercise number 1 simulates the airflow around the airfoil and creates a water film (Icing) on the surface of the airfoil body. In fact, when moisturized air and water droplets hit the surface of the airfoil, a water film may form on the airfoil surface. The purpose of this work is to investigate the thickness of the produced and flowing fluid layer on the airfoil body.

### MRF (Frame Motion)

In project number 2, the airflow passing over an impeller of an electrical motor is investigated. The airflow enters the computational domain with 80m/s, and the impeller rotates at 1000rpm. A Realizable k-epsilon model is exploited to solve turbulent flow equations. It should be noted that the MRF (frame motion) option has been activated to model the rotation of the impeller.

### LES

problem number 3 simulates compressible flow around an aerial structure by applying Large Eddy Simulation (LES). A density-based approach has been used to define the type of airflow solution around this aerial structure; Because the existing airflow is entirely compressible. This acoustic project (practical exercise number 5), simulates sound pressure waves around cylinders in 4 different positions (4 cases). Definitive density is equivalent to air density, i.e., 1.225 kg / m3, the velocity of air is 69.2 m/s, and the LES Smagorinsky model is used to simulate turbulence of flow. Also, Ffowcs-Williams & Hawking’s equations are used to model acoustic

### Aerospace Flow Control

In study number 4, we employed a wing plane airfoil and evaluated the stall angle. Also, the air is assumed to be incompressible and isothermal. The geometry is a 3-meter airfoil inside a 60-meter wind tunnel. Also, the maximum speed of 10 m/s is selected for the inlet.

### Inviscid

In project number 6, supersonic flow over an F-16 aircraft considering inviscid fluid was simulated, and then the results were investigated. Supersonic speed is the speed of an object that exceeds the speed of sound. It is estimated to be around 343 m/s in the dry air at a temperature of 20 C.

### MHD

Issue number 7 concerns the simulation of airflow around a NACA 0015 airfoil. This airfoil is a symmetrical airfoil that does not produce a lift force at zero attack angle, and we investigate the lift coefficient of this airfoil at different attack angles with and without magnetic force (MHD). In this problem, we study the separation and the maximum angle of attack where the separation does not occur.

### Aerodynamic Paper Validation

In project number 8, we simulated the compressible flow around the NACA0012 airfoil, and then we compared the results with the results extracted from an article called this “Numerical Simulation OF VISCOUS TRANSONIC AIRFOIL FLOWS.” The solver is density-based due to compressibility. By comparing the simulation results with the results in the article, it can be concluded that the simulation has been validated with the article so accurately.

### FSI

Problem number 9 simulates the airflow around an airfoil using the Fluid Solid Interaction (FSI) method. In this simulation, a circular computational domain of ​​airflow is designed; So that an airfoil is located in this area. Due to the fact that this airfoil is moving in the air at a considerable speed, the airflow collides with its body and exerts a force on it.

### Acoustic & LES

Finally, practical exercise number 10 simulates the airflow inside a turbojet (intake fan) and examines the acoustic wave and the sound produced inside this turbojet. The model includes a turbojet that has a fan in its inlet. This fan is rotating at 2000 rpm and around the X-axis in the current model.

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