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An axial compressor is a gas compressor that can continuously pressurize gases. It is a rotating, airfoil-based compressor in which the gas or working fluid principally flows parallel to the axis of rotation, or axially. This differs from other rotating compressors such as centrifugal compressors, axi-centrifugal compressors and mixed-flow compressors where the fluid flow will include a "radial component" through the compressor. The energy level of the fluid increases as it flows through the compressor due to the action of the rotor blades which exert a torque on the fluid. The stationary blades slow the fluid, converting the circumferential component of flow into pressure. Compressors are typically driven by an electric motor or a steam or a gas turbine.
Axial flow compressors produce a continuous flow of compressed gas, and have the benefits of high efficiency and large mass flow rate, particularly in relation to their size and cross-section. They do, however, require several rows of airfoils to achieve a large pressure rise, making them complex and expensive relative to other designs (e.g. centrifugal compressors).
Axial compressors are integral to the design of large gas turbines such as jet engines, high speed ship engines, and small scale power stations. They are also used in industrial applications such as large volume air separation plants, blast furnace air, fluid catalytic cracking air, and propane hydrogenation. Due to high performance, high reliability and flexible operation during the flight envelope, they are also used in aerospace engines.

Premier essai de simulation du modular DC

The dynamic flows of a plane( aerodynamic) including heat transfer

El objetivo simular la turbulencia de un liquido por la válvula

Final semester Graduation Thesis Project.

The goal is to show the fluid flow  through a water turbine using CFD simulation

Simulation of incrompressible fluid flow to maximum

Testing the lattice fin designs on reusable rockets.

Examine Effects of baffles in a turbulent system

The goal of the project is to optimize the design of an F1 Rear wing. An incompressible flow simulation will be used with a speed of 200 km/h at the inlet and on the floor. F1 Rear wings are designed to create more negative lift on the car by deflecting the incoming air and creating flow separation. This serves to reduce the amount of drag experienced by the vehicle which allows to it move faster in a given distance than a vehicle that doesn't possess one.

CFD external flow case study for fluid mechanics I. The optimization of drag at low Reynolds numbers on snack food shapes.

To find the velocity and pressure contours at low Re number

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