Aerodynamic & Aerospace ANSYS Fluent Training Package, Beginner

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-D 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 using ANSYS Fluent 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.