Mohd. Jaafar, Mohammad Nazri and N. I., Kamarudin and M., Hanafi and A. R., Mantari (2010) Development of air supply system for gas turbine combustor test rig. In: 10th Asian International Conference On Fluid Machinery, 2010, Kuala Lumpur, Malaysia.
Official URL: http://dx.doi.org/10.1063/1.3464939
Complete combustion process occurs when the air and fuel burns at their stoichiometric ratio, which determines the appropriate amount of air needed to be supplied to the combustion chamber. Thus, designing an appropriate air supply system is important, especially for multi-fuel combustion. Each type of fuel has different molecular properties and structures which influence the stoichiometric ratio. Therefore, the designed air supply system must be operable for different types of fuels. Basically, the design of the air supply system is at atmospheric pressure. It is important that the air which enters the combustion chamber is stable and straight. From the calculation, the maximum required mass flow rate of air is 0.1468kg/s.
|Item Type:||Conference or Workshop Item (Paper)|
|Uncontrolled Keywords:||flow measurement, compressors, thermal expansion, viscosity, bioenergy conversion, velocity measurements, modulators and demodulators, discriminators, comparators, mixers, limiters, and compressors, thermal expansion, thermomechanical effects, viscous and viscoelastic instabilities|
|Subjects:||T Technology > TJ Mechanical engineering and machinery|
|Deposited By:||Liza Porijo|
|Deposited On:||27 Jul 2012 07:45|
|Last Modified:||27 Jul 2012 07:45|
Repository Staff Only: item control page