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TITLE : DESIGN OF A GAS TURBINE COMBUSTOR UNDER AERODYNAMIC CONSIDERATIONS  
AUTHORS : Selvakumaran. T      Kadiresh P.N.            
DOI : http://dx.doi.org/10.18000/ijodam.70106  
ABSTRACT :

A theoretical design of a tubular type gas turbine combustor design was carried out in this paper in aerodynamic design point of view. Aerodynamic design processes plays a vital role in the design and performance of gas turbine combustion systems. With good aerodynamic design and good matching fuel-injection system, a trouble free combustor design may be arrived. By considering the inlet parameters such as pressure, temperature, density and air mass flow rate of a combustor, a design process was carried out. Design process involves the geometric dimensional calculations of various geometries in a combustor like casing cross-sectional area and its length, linear cross-sectional area and its length, swirler design calculations, etc. Thermodynamically, ideal constant pressure process takes place inside a combustor.

 
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