contributor author | Zhang, Xu | |
contributor author | Yi, Ran | |
contributor author | Chen, C. P. | |
date accessioned | 2022-02-05T22:22:43Z | |
date available | 2022-02-05T22:22:43Z | |
date copyright | 3/15/2021 12:00:00 AM | |
date issued | 2021 | |
identifier issn | 0742-4795 | |
identifier other | gtp_143_06_061009.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4277430 | |
description abstract | In this study, a model flame of quasi-one-dimensional (1D) counterflow spray flame has been developed. The two-dimensional (2D) multiphase convection-diffusion-reaction equations have been simplified to one dimension using similarity reduction under the Eulerian framework. This model flame is able to directly account for nonadiabatic heat loss, preferential evaporation, as well as multiple combustion regimes present in realistic spray combustion processes. A spray flamelet library was generated based on the model flame. To retrieve data from the spray flamelet library, the enthalpy was used as an additional controlling variable to represent the interphase heat transfer, while the mixing and chemical reaction processes were mapped to the mixture fraction and the progress variable. The spray flamelet generated manifolds (SFGM) approach was validated against the results from the direct integration of finite rate chemistry as a benchmark. The SFGM approach was found to give a better performance in terms of predictions of temperature and species mass fractions. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Development of a Multiphase Flamelet Generated Manifold for Spray Combustion Simulations | |
type | Journal Paper | |
journal volume | 143 | |
journal issue | 6 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4050338 | |
journal fristpage | 061009-1 | |
journal lastpage | 061009-10 | |
page | 10 | |
tree | Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 006 | |
contenttype | Fulltext | |