PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS
Abstract
This paper presents the preliminary design methodology for a Reverse flow annular combustor based on calculation of the geometric parameters, gas temperature profile, liner wall temperatures and position of air admission holes for a small gas turbine engine with Jet A as fuel. It also includes the modelling and numerical simulation of temperature distribution at centerline, inlet and outlet of the combustor using Ansys-CFX, carried out at basic design point operating conditions.
Keywords
Reverse flow annular combustor, numerical simulation, Ansys-CFX, operating conditions
Citations
IRE Journals:
DEEPA M S , Dr. A AROKKIASWAMY
"PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS" Iconic Research And Engineering Journals Volume 2 Issue 4 2018 Page 17-22
IEEE:
DEEPA M S , Dr. A AROKKIASWAMY
"PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS" Iconic Research And Engineering Journals, 2(4)
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