Measurement and Simulation of Turbulent Mixing in a Jet in CrossflowSource: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 006::page 61504Author:Flavio Cesar Cunha Galeazzo
,
Richard J. Valdes
,
Werner Krebs
,
Georg Donnert
,
Peter Habisreuther
,
Nikolaos Zarzalis
DOI: 10.1115/1.4002319Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Computational fluid dynamics (CFD) has an important role in current research. While large eddy simulations (LES) are now common practice in academia, Reynolds-averaged Navier–Stokes (RANS) simulations are still very common in the industry. Using RANS allows faster simulations, however, the choice of the turbulence model has a bigger impact on the results. An important influence of the turbulence modeling is the description of turbulent mixing. Experience has shown that often inaccurate simulations of combustion processes originate from an inadequate description of the mixing field. A simple turbulent flow and mixing configuration of major theoretical and practical importance is the jet in crossflow (JIC). Due to its good fuel-air mixing capability over a small distance, JIC is favored by gas turbine manufacturers. As the design of the mixing process is the key to creating stable low NOx combustion systems, reliable predictive tools and detailed understanding of this basic system are still demanded. Therefore, the current study has re-investigated the JIC configuration under engine relevant conditions both experimentally and numerically using the most sophisticated tools available today. The combination of planar particle image velocimetry and laser induced fluorescence was used to measure the turbulent velocity and concentration fields as well as to determine the correlations of the Reynolds stress tensor ui′uj′¯ and the Reynolds flux vector ui′c′¯. Boundary conditions were determined using laser Doppler velocimetry. The comparisons between the measurements and simulation using RANS and LES showed that the mean velocity field was well described using the SST turbulence model. However, the Reynolds stresses and more so, the Reynolds fluxes deviate substantially from the measured data. The systematic variation of the turbulent Schmidt number reveals the limited influence of this parameter indicating that the basic modeling is amiss. The results of the LES simulation using the standard Smagorinsky model were found to provide much better agreement with the experiments also in the description of turbulent mixing.
keyword(s): Turbulence , Engineering simulation , Measurement , Reynolds-averaged Navier–Stokes equations , Simulation , Stress AND Boundary-value problems ,
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contributor author | Flavio Cesar Cunha Galeazzo | |
contributor author | Richard J. Valdes | |
contributor author | Werner Krebs | |
contributor author | Georg Donnert | |
contributor author | Peter Habisreuther | |
contributor author | Nikolaos Zarzalis | |
date accessioned | 2017-05-09T00:43:38Z | |
date available | 2017-05-09T00:43:38Z | |
date copyright | June, 2011 | |
date issued | 2011 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-27165#061504_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/146008 | |
description abstract | Computational fluid dynamics (CFD) has an important role in current research. While large eddy simulations (LES) are now common practice in academia, Reynolds-averaged Navier–Stokes (RANS) simulations are still very common in the industry. Using RANS allows faster simulations, however, the choice of the turbulence model has a bigger impact on the results. An important influence of the turbulence modeling is the description of turbulent mixing. Experience has shown that often inaccurate simulations of combustion processes originate from an inadequate description of the mixing field. A simple turbulent flow and mixing configuration of major theoretical and practical importance is the jet in crossflow (JIC). Due to its good fuel-air mixing capability over a small distance, JIC is favored by gas turbine manufacturers. As the design of the mixing process is the key to creating stable low NOx combustion systems, reliable predictive tools and detailed understanding of this basic system are still demanded. Therefore, the current study has re-investigated the JIC configuration under engine relevant conditions both experimentally and numerically using the most sophisticated tools available today. The combination of planar particle image velocimetry and laser induced fluorescence was used to measure the turbulent velocity and concentration fields as well as to determine the correlations of the Reynolds stress tensor ui′uj′¯ and the Reynolds flux vector ui′c′¯. Boundary conditions were determined using laser Doppler velocimetry. The comparisons between the measurements and simulation using RANS and LES showed that the mean velocity field was well described using the SST turbulence model. However, the Reynolds stresses and more so, the Reynolds fluxes deviate substantially from the measured data. The systematic variation of the turbulent Schmidt number reveals the limited influence of this parameter indicating that the basic modeling is amiss. The results of the LES simulation using the standard Smagorinsky model were found to provide much better agreement with the experiments also in the description of turbulent mixing. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Measurement and Simulation of Turbulent Mixing in a Jet in Crossflow | |
type | Journal Paper | |
journal volume | 133 | |
journal issue | 6 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.4002319 | |
journal fristpage | 61504 | |
identifier eissn | 0742-4795 | |
keywords | Turbulence | |
keywords | Engineering simulation | |
keywords | Measurement | |
keywords | Reynolds-averaged Navier–Stokes equations | |
keywords | Simulation | |
keywords | Stress AND Boundary-value problems | |
tree | Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 006 | |
contenttype | Fulltext |