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# Aerodynamic & Aerospace ANSYS Fluent Training Package, Beginner

\$420.00 Student Discount

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 BEGINNER level.

#### Intake of Jet Engine CFD Simulation by ANSYS Fluent Tutorial

• The problem numerically simulates airflow in Jet Intake using ANSYS Fluent software.
• We design the 3-D model by the Design ModelerÂ software.
• We Mesh the model by ANSYS Meshing software, and the element number equalsÂ 389136.

#### Spoiler Modes Comparison for F1 Car Aerodynamics

• The problem numerically simulates Spoiler Modes Comparison for F1 Car Aerodynamics using ANSYS Fluent software.
• We design the 3-D model by the Design ModelerÂ software.
• We Mesh the model by ANSYS Meshing software, and the polyhedral element number equals 450000.
• We aim to compare the open and close modes of the spoiler and observe the difference between the lift and drag forces.

#### Rotating Disk Effect on Surrounding Airflow, Moving Wall

• The problem numerically simulates Rotating Disk in a room using ANSYS Fluent software.
• We design the 3-D model by the Design ModelerÂ software.
• We Mesh the model by ANSYS Meshing software, and the element number equalsÂ 716870.
• We use the Moving WallÂ for the disk to define the rotational movement.

#### Slot Effect on Wing Aerodynamic Performance, ANSYS Fluent Simulation Training

• The problem numerically simulates airflow over an airfoil (NACA4421) with a slot on the leading edge using ANSYS Fluent software.
• We design the 2-D model by the Design ModelerÂ software.
• We Mesh the model by ANSYS Meshing software, and the element number equalsÂ 260000.
• We aim to study the aerodynamic performance of the wing (drag and lift).

#### Cooling of Airfoil Surface by Lateral Hole Air Inlets

• The problem numerically simulates Cooling of Airfoil Surface by Lateral Hole Air Inlets using ANSYS Fluent software.
• We design the 3-D model by the Design ModelerÂ software.
• We Mesh the model by ANSYS Meshing software, and the element number equalsÂ 582263.
• The Energy Equation is activated to define the cooling process.

#### NACA 0012 Airfoil, Compressible Flow) CFD Simulation

• The problem numerically simulates NACA 0012 Airfoil (Compressible Flow) using ANSYS Fluent software.
• We design the 2-D model by the Design ModelerÂ 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.

#### Shock Wave in a Supersonic Airflow, Transient Solver

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

#### 3-D Airfoil CFD Simulation, ANSYS Fluent Training

This project will study an incompressible isothermal air flow adjacent to a 3-D airfoil.

#### Aerospike CFD Simulation Considering Shock Wave

• The problem numerically simulates an Aerospike Considering Shock Wave using ANSYS FluentÂ software.
• We design the 3-D model by theÂ Design ModelerÂ software.
• Mesh grid is generated using ANSYS Meshing, and the element number equals 153,987.
• k-Omega SST turbulence model is used to capture the shock wave.

#### Airflow on the Dimpled Rotating Cylinder CFD Simulation

• The problem numerically simulates Airflow on the Dimpled Rotating Cylinder using ANSYS Fluent software.
• We design the 3-D model with the Design ModelerÂ software.
• We mesh the model with ANSYS Meshing software, and the element number equalsÂ 1064903.
• We use the Frame Motion method to define the rotational movement.

## Aerodynamic & Aerospace ANSYS Fluent CFD Simulation Training Package for BEGINNERS

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 BEGINNER level.

ANSYS Fluent software simulates the airflow in a three-dimensional jet intake as practical exercise number 1. Jet engines are the primary and most commonly used thruster in aerodynamics. Every Jet engine includes an intake section similar to the present exercise, which is used for subsonic and supersonic flows.

Project number 2 is going to study an incompressible isothermal air flow adjacent to a 3-DÂ airfoil. The geometry is a 1-meter airfoil inside a 20-meter wind tunnel. Also, the maximum speed of 10 m/s is selected for the inlet.

In practical exercise, number 3, an aerospike, has been simulated. The flow inlet has a pressure of 2000000 Pa and a temperature of 900 K. Also, the boundary condition of the pressure outlet is 50000 Pa, and the simulation is performed as axisymmetric.

In project number 4, ANSYS Fluent software investigates steady airflow over an airfoil (NACA4421). Airfoil has a shape deformity called the slot, which separates it into two parts. A slot in the airfoil industry is used to optimize airfoil performance, including increased lift force.

Also, practical exercise number 5 simulates a rotating disk in a room usingÂ ANSYS FluentÂ software. This work aims to investigate the airflow behavior under the influence of the rotational motion of a rotating disk. In this simulation, there is airflow in a computational domain of a room, and in the middle of this room, a rotating disk with a certain rotational speed is placed.

In training number 6, the movement of heated airflow over the surface of an airfoil and the surface cooling of the mentioned airfoil using lateral hole air inlets is simulated. The heated air enters the computational. Two lateral air inlets are responsible for the airfoil cooling of the blade or airfoil.

Then, as practical exercise number 7, we compare two different spoilers in opening and closing modes. The car, as a moving device, has always been involved with airflow, so the science of aerodynamics has helped engineers bring the best performance to the vehicle.

Problem number 8 is going to simulate airflow in a rectangular channel passing through a rotating dimpled cylinder. A cylindrical object is placed in the channel. The airflow enters the rectangular channel at a horizontal velocity of 0.45 m / s, and it collides with the cylindrical body.

Project number 9 is going to simulate a NACA0012 airfoil in compressible airflow. Geometric defining parameters include chord line, angle of attack, leading edge, and trailing edge. The direction of the airflow into the airfoil body is defined by the angle of attack (the angle between the chord and the horizontal direction of the airflow velocity).

Finally, project number 10 simulates the supersonic airflow encountered by a two-way oblique airfoil barrier passing through a channel, thus investigating fluid behavior and creating a shock wave phenomenon. The airflow in the simulation environment around the obstacles and canals has a temperature of 129.46 Kelvin and a Mach number of 2.49, and the direction of the airflow is generally assumed to be in the same direction. Since the airflow in this model is supersonic, it has a larger Mach number than 1.

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