Swirling flows provide intensive mixing in a small volume in addition to flame stabilization by the formation of a central recirculation zone which back-circulates heat. A numerical study of unsteady isothermal flow in a pilot scale pulverized- fuel swirl combustor has been performed using the standard k − epsilon turbulence model and Reynolds stress model (RSM). The objective of this work is to compare the numerical predictions of the two turbulence models. The precession is induced by a tangential inlet, for primary air, and guide vanes, for secondary air. A sequence of CFD solutions on successively finer meshes is examined and the order of accuracy of the solutions is estimated by Richardson extrapolation. The results for a Reynolds number of 54 425 and 76 400, swirl number of 0.78 and 0.82 for primary and secondary air, respectively, show the presence of a large and asymmetric region corresponding to the precessing vortex core. Moreover, spiral and bubble type vortex breakdown have been observed and their frequencies analyzed by the monitored of velocities using Fast Fourier Transform (FFT).
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Swirling flows provide intensive mixing in a small volume in addition to flame stabilization by the formation of a central recirculation zone which back-circulates heat. A numerical study of unsteady isothermal flow in a pilot scale pulverized- fuel swirl combustor has been performed using the standard k − epsilon turbulence model and Reynolds stress model (RSM). The objective of this work is to compare the numerical predictions of the two turbulence models. The precession is induced by a tangential inlet, for primary air, and guide vanes, for secondary air. A sequence of CFD solutions on successively finer meshes is examined and the order of accuracy of the solutions is estimated by Richardson extrapolation. The results for a Reynolds number of 54 425 and 76 400, swirl number of 0.78 and 0.82 for primary and secondary air, respectively, show the presence of a large and asymmetric region corresponding to the precessing vortex core. Moreover, spiral and bubble type vortex breakdown have been observed and their frequencies analyzed by the monitored of velocities using Fast Fourier Transform (FFT).
Juan Antonio Ramirez Vazquez, Ph. D.: Studied Energy Efficiency and Renewable Energies at University of Zaragoza, Spain. Assistant Professor at University of Guanajuato, Mexico.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Swirling flows provide intensive mixing in a small volume in addition to flame stabilization by the formation of a central recirculation zone which back-circulates heat. A numerical study of unsteady isothermal flow in a pilot scale pulverized- fuel swirl combustor has been performed using the standard k _ epsilon turbulence model and Reynolds stress model (RSM). The objective of this work is to compare the numerical predictions of the two turbulence models. The precession is induced by a tangential inlet, for primary air, and guide vanes, for secondary air. A sequence of CFD solutions on successively finer meshes is examined and the order of accuracy of the solutions is estimated by Richardson extrapolation. The results for a Reynolds number of 54 425 and 76 400, swirl number of 0.78 and 0.82 for primary and secondary air, respectively, show the presence of a large and asymmetric region corresponding to the precessing vortex core. Moreover, spiral and bubble type vortex breakdown have been observed and their frequencies analyzed by the monitored of velocities using Fast Fourier Transform (FFT). 92 pp. Englisch. N° de réf. du vendeur 9783639861235
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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Ramirez-Vazquez Juan A.Juan Antonio Ramirez Vazquez, Ph. D.: Studied Energy Efficiency and Renewable Energies at University of Zaragoza, Spain. Assistant Professor at University of Guanajuato, Mexico.Swirling flows provide intens. N° de réf. du vendeur 151404782
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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Swirling flows provide intensive mixing in a small volume in addition to flame stabilization by the formation of a central recirculation zone which back-circulates heat. A numerical study of unsteady isothermal flow in a pilot scale pulverized- fuel swirl combustor has been performed using the standard k ¿ epsilon turbulence model and Reynolds stress model (RSM). The objective of this work is to compare the numerical predictions of the two turbulence models. The precession is induced by a tangential inlet, for primary air, and guide vanes, for secondary air. A sequence of CFD solutions on successively finer meshes is examined and the order of accuracy of the solutions is estimated by Richardson extrapolation. The results for a Reynolds number of 54 425 and 76 400, swirl number of 0.78 and 0.82 for primary and secondary air, respectively, show the presence of a large and asymmetric region corresponding to the precessing vortex core. Moreover, spiral and bubble type vortex breakdown have been observed and their frequencies analyzed by the monitored of velocities using Fast Fourier Transform (FFT).VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 92 pp. Englisch. N° de réf. du vendeur 9783639861235
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Swirling flows provide intensive mixing in a small volume in addition to flame stabilization by the formation of a central recirculation zone which back-circulates heat. A numerical study of unsteady isothermal flow in a pilot scale pulverized- fuel swirl combustor has been performed using the standard k _ epsilon turbulence model and Reynolds stress model (RSM). The objective of this work is to compare the numerical predictions of the two turbulence models. The precession is induced by a tangential inlet, for primary air, and guide vanes, for secondary air. A sequence of CFD solutions on successively finer meshes is examined and the order of accuracy of the solutions is estimated by Richardson extrapolation. The results for a Reynolds number of 54 425 and 76 400, swirl number of 0.78 and 0.82 for primary and secondary air, respectively, show the presence of a large and asymmetric region corresponding to the precessing vortex core. Moreover, spiral and bubble type vortex breakdown have been observed and their frequencies analyzed by the monitored of velocities using Fast Fourier Transform (FFT). N° de réf. du vendeur 9783639861235
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Taschenbuch. Etat : Neu. Flow Dynamics in a Swirl Combustion System | Juan A. Ramirez-Vazquez (u. a.) | Taschenbuch | 92 S. | Englisch | 2015 | Scholars' Press | EAN 9783639861235 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. N° de réf. du vendeur 104110032
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