Beta
195199

Parametric study for reducing emission characteristics using different computational schemes

Article

Last updated: 04 Jan 2025

Subjects

-

Tags

-

Abstract

The present study numerically predicts emissions (NOx & CO) characteristics issued from swirl burner using different computational schemes adopted in ANSYS 17.2. Various turbulence models were tested and compared in a structured grid having an average skewness of 0.04. RSM model shows the best results in predicting the central toroidal recirculation zone for such severe swirling flow (S>0.6). Three different schemes of combustion modeling were also tested and compared. Flamelet PDF model was preferred among other combustion models for its potential to consider non-equilibrium chemistry, where its choice was recommended form many studies in the literature. A radiation heat transfer analysis was carried out using P1 radiation model to account radiation effects in estimating NOx and CO concentrations. The effect of varying swirl ratio, excess air, diluting fuel with N2 and CO2, oxidizer preheating, and oxidizer composition on emissions (NOx and CO) reduction strategy concluded that increasing the swirl number, excess air factor, and (N2 and CO2) mixing ratios have a considerable influence on NOx and CO emissions reduction. While increasing the preheating temperature, and the oxidizer Oxygen concentration leads to an increase the NOx and CO emissions. Hence, a considerable reduction in NOx and CO formation was apparently observed by lowering the peak flame temperature less than 1800 K. These predicted outcomes are in agreement with measurements data published in the literature.

DOI

10.1088/1757-899X/610/1/012041

Keywords

NOx Emission, Turbulent Combustion, Modelling

Authors

First Name

Hatem

Last Name

Kayed

MiddleName

-

Affiliation

Department of Mechanical Power Engineering, Cairo University, Egypt.

Email

-

City

-

Orcid

-

Volume

18

Article Issue

18

Related Issue

27598

Issue Date

2019-04-01

Receive Date

2021-09-19

Publish Date

2019-04-01

Page Start

1

Page End

17

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_195199.html

Detail API

https://asat.journals.ekb.eg/service?article_code=195199

Order

43

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

Parametric study for reducing emission characteristics using different computational schemes

Details

Type

Article

Created At

22 Jan 2023