Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades

The ability to accurately predict the effect of cooling on gas turbine blades is essential in designing the blades that will operate at extremely high temperature. The standard k-? linear eddy viscosity model is known to be inaccurate in predicting highly complex flows. Thus, a relatively new cubic...

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Main Author: Mostafa N.A.
Other Authors: 24332354200
Format: Conference paper
Published: 2023
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spelling my.uniten.dspace-308282023-12-29T15:54:07Z Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades Mostafa N.A. 24332354200 Cubic Eddy viscosity model Flat surface Jet impingement Non-linear Numerical investigation Forecasting Gas turbine locomotives Gas turbines Heat exchangers Heat transfer Kinetic energy Sustainable development Turbomachine blades Turbulent flow Viscosity Wall flow Eddy viscosity model Flat surfaces Jet impingement Non-linear Numerical investigations Mathematical models The ability to accurately predict the effect of cooling on gas turbine blades is essential in designing the blades that will operate at extremely high temperature. The standard k-? linear eddy viscosity model is known to be inaccurate in predicting highly complex flows. Thus, a relatively new cubic k-? nonlinear eddy viscosity model was tested to ascertain whether it has improved the performance of eddy viscosity models. A single jet impingement on a flat plate with surface-to-nozzle distance of H/D = 6 was investigated numerically using a cubic k-? nonlinear eddy viscosity model of Craft et. al. [1] and high-Re k-? linear eddy viscosity model of Jones & Launder [2]. Both use standard wall-function to model the near-wall flow. Dynamic field profiles taken at certain distances away from the impingement point were compared with experimental results of Cooper et al. [3]. The heat transfer field results were compared with the experimental data of Baughn et al. [4]. The dynamic field results show that the cubic non-linear model gives a much better prediction than the linear model. The heat transfer results showed that the linear model over-predicted the heat transfer rate at the stagnation point whilst the non-linear model gave under-prediction due to a lower prediction of the turbulent kinetic energy at that region. �2009 IEEE. Final 2023-12-29T07:54:07Z 2023-12-29T07:54:07Z 2009 Conference paper 10.1109/ICEENVIRON.2009.5398641 2-s2.0-77949615353 https://www.scopus.com/inward/record.uri?eid=2-s2.0-77949615353&doi=10.1109%2fICEENVIRON.2009.5398641&partnerID=40&md5=9d4cd1f483196429cea2f55df35a4e82 https://irepository.uniten.edu.my/handle/123456789/30828 5398641 226 231 Scopus
institution Universiti Tenaga Nasional
building UNITEN Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Tenaga Nasional
content_source UNITEN Institutional Repository
url_provider http://dspace.uniten.edu.my/
topic Cubic
Eddy viscosity model
Flat surface
Jet impingement
Non-linear
Numerical investigation
Forecasting
Gas turbine locomotives
Gas turbines
Heat exchangers
Heat transfer
Kinetic energy
Sustainable development
Turbomachine blades
Turbulent flow
Viscosity
Wall flow
Eddy viscosity model
Flat surfaces
Jet impingement
Non-linear
Numerical investigations
Mathematical models
spellingShingle Cubic
Eddy viscosity model
Flat surface
Jet impingement
Non-linear
Numerical investigation
Forecasting
Gas turbine locomotives
Gas turbines
Heat exchangers
Heat transfer
Kinetic energy
Sustainable development
Turbomachine blades
Turbulent flow
Viscosity
Wall flow
Eddy viscosity model
Flat surfaces
Jet impingement
Non-linear
Numerical investigations
Mathematical models
Mostafa N.A.
Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades
description The ability to accurately predict the effect of cooling on gas turbine blades is essential in designing the blades that will operate at extremely high temperature. The standard k-? linear eddy viscosity model is known to be inaccurate in predicting highly complex flows. Thus, a relatively new cubic k-? nonlinear eddy viscosity model was tested to ascertain whether it has improved the performance of eddy viscosity models. A single jet impingement on a flat plate with surface-to-nozzle distance of H/D = 6 was investigated numerically using a cubic k-? nonlinear eddy viscosity model of Craft et. al. [1] and high-Re k-? linear eddy viscosity model of Jones & Launder [2]. Both use standard wall-function to model the near-wall flow. Dynamic field profiles taken at certain distances away from the impingement point were compared with experimental results of Cooper et al. [3]. The heat transfer field results were compared with the experimental data of Baughn et al. [4]. The dynamic field results show that the cubic non-linear model gives a much better prediction than the linear model. The heat transfer results showed that the linear model over-predicted the heat transfer rate at the stagnation point whilst the non-linear model gave under-prediction due to a lower prediction of the turbulent kinetic energy at that region. �2009 IEEE.
author2 24332354200
author_facet 24332354200
Mostafa N.A.
format Conference paper
author Mostafa N.A.
author_sort Mostafa N.A.
title Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades
title_short Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades
title_full Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades
title_fullStr Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades
title_full_unstemmed Numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades
title_sort numerical investigation of a single jet impingement on a flat surface using a cubic k-? non-linear eddy viscosity model, to predict the effect of cooling on gas turbine blades
publishDate 2023
_version_ 1806427573481111552
score 13.214268