Flow and Heat Transfer in a Ribbed Converging-Diverging U-Duct Under Rotating and Non-Rotating ConditionsSource: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003::page 31005-1Author:Kim, Wanjae
,
Shih, Tom I-P.
,
Dalton, Richard P.
,
Bryden, Kenneth Mark
,
Chang, Sung Yong
,
Park, Gyu Sang
DOI: 10.1115/1.4066567Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A numerical study based on steady Reynolds-averaged-Navier–Stokes (RANS) with the shear stress transport (SST) turbulence model was performed to investigate the flow and heat transfer in a ribbed U-duct with a rectangular cross section that converges linearly in the radially outward direction and diverges linearly in the radially inward direction under rotating and nonrotating conditions. Parameters examined include rotation number (Roi = 0, 0.0219, 0.0336, 0.0731), Reynolds number (Rei = 46,000, 100,000, and 154,000), and the duct's taper angle (α = 0 deg and 1.41 deg) under conditions relevant to gas turbines used for electric power generation. Results obtained show that increasing the taper angle from 0 deg to 1.41 deg, which appears negligibly small, significantly increases both the friction coefficient and the Nusselt number whether there is rotation or not. With rotation at Roi = 0.0336 and Rei = 100,000, the maximum increase in the average friction coefficient and Nusselt number was found to be 41.7% and 36.6%, respectively. Without rotation at Rei = 46,000, those are 11.5% and 14.7%, respectively.
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contributor author | Kim, Wanjae | |
contributor author | Shih, Tom I-P. | |
contributor author | Dalton, Richard P. | |
contributor author | Bryden, Kenneth Mark | |
contributor author | Chang, Sung Yong | |
contributor author | Park, Gyu Sang | |
date accessioned | 2025-04-21T10:06:46Z | |
date available | 2025-04-21T10:06:46Z | |
date copyright | 10/14/2024 12:00:00 AM | |
date issued | 2024 | |
identifier issn | 0889-504X | |
identifier other | turbo_147_3_031005.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4305519 | |
description abstract | A numerical study based on steady Reynolds-averaged-Navier–Stokes (RANS) with the shear stress transport (SST) turbulence model was performed to investigate the flow and heat transfer in a ribbed U-duct with a rectangular cross section that converges linearly in the radially outward direction and diverges linearly in the radially inward direction under rotating and nonrotating conditions. Parameters examined include rotation number (Roi = 0, 0.0219, 0.0336, 0.0731), Reynolds number (Rei = 46,000, 100,000, and 154,000), and the duct's taper angle (α = 0 deg and 1.41 deg) under conditions relevant to gas turbines used for electric power generation. Results obtained show that increasing the taper angle from 0 deg to 1.41 deg, which appears negligibly small, significantly increases both the friction coefficient and the Nusselt number whether there is rotation or not. With rotation at Roi = 0.0336 and Rei = 100,000, the maximum increase in the average friction coefficient and Nusselt number was found to be 41.7% and 36.6%, respectively. Without rotation at Rei = 46,000, those are 11.5% and 14.7%, respectively. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Flow and Heat Transfer in a Ribbed Converging-Diverging U-Duct Under Rotating and Non-Rotating Conditions | |
type | Journal Paper | |
journal volume | 147 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4066567 | |
journal fristpage | 31005-1 | |
journal lastpage | 31005-15 | |
page | 15 | |
tree | Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003 | |
contenttype | Fulltext |