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Co2 Mass Fraction Min
Co2 Mass Fraction-min
Masot Mass Fraction-min
N2 Mass Fraction-min
O2 Mass Fraction-min
Pathline-min
Pressure-min
Temperature-min
Velocity Vector-min
Velocity-min
Co2 Mass Fraction MinMasot Mass Fraction MinN2 Mass Fraction MinO2 Mass Fraction MinPathline MinPressure MinTemperature MinVelocity Vector MinVelocity Min

Project Description

In the last twenty years there has been a huge growth in use of gas turbines in the industry, in power plants, air planes and rackets. The efficiency of gas turbines impact on fuel usage and high efficient gas turbines will reduce our costs. Different parts of gas turbines are: intake for air, compressor to raise the pressure, combustor or combustion chamber in which air and fuel are mixed and burned, Turbine to extract the energy and exhaust. To increase the efficiency of a gas turbine system or gas turbine engine we have to investigate each part separately. Combustion is one of the most important processes occurring in combustor. The flow in combustion chamber is classified as reacting flows. Therefore, the design of combustion chamber is of great importance. CFD simulations are necessary to investigate how the fuel is burned and analyze the flow patterns, distribution of air. The results of these simulations reduce the cost of product design and will have crucial effects on improvement of our environment.

Project Details

TITLE: CFD SIMULATION OF GAS TURBINE COMBUSTION CHAMBER

PROJECT TYPE: COMBUSTION AND REACTION

MODULE: SPECIES TRANSPORT

TIME: 6 WEEKS

PRICE: 1400 $

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