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PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS
Subject area: Science,Engineering and Technology · Area of research: AEROSPACE AND AERONAUTICAL ENGINEERING
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
How to cite this paper
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
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, vol. 2, no. 4, Oct. 2018
DEEPA M S, Dr. A AROKKIASWAMY (2018). PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS. Iconic Research And Engineering Journals, 2(4).
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, vol. 2, no. 4, Oct. 2018.
@article{1700761,
author = {DEEPA M S, Dr. A AROKKIASWAMY},
title = {PRELIMINARY DESIGN AND NUMERICAL SIMULATION OF A REVERSE FLOW ANNULAR COMBUSTOR AT BASIC DESIGN POINT OPERATING CONDITIONS},
journal = {Iconic Research And Engineering Journals},
year = {2018},
volume = {2},
number = {4},
pages = {17-22},
issn = {2456-8880},
url = {https://www.irejournals.com/formatedpaper/1700761.pdf},
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},
month = {October},
}