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    Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 008::page 81006-1
    Author:
    Wang, Hanlin
    ,
    Klein, Denali
    ,
    Wright, Lesley M.
    DOI: 10.1115/1.4067322
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This study investigates the effect of acceleration and deceleration in the turn region of a two-pass, serpentine channel. Channel aspect ratios of 2:1 and 4:1 are considered in three combinations to investigate the effect of acceleration and deceleration through the turn region in a smooth, two-pass channel. For each aspect ratio combination, the experiments include Reynolds numbers ranging from 15,000 to 45,000 in the first passage and from 9,000 to 75,000 in the second pass. Surface heat transfer coefficient (h) distributions are measured by transient thermochromic liquid crystal technique, and the flow field characteristics are measured by tomographic PIV. Enhanced heat transfer on the side wall and downstream in the second pass is observed for all cases. Based on the first-pass Nusselt number (Nu) ratio, the accelerating case provides the best heat transfer enhancement. However, based on the second-pass Nu ratio, the decelerating case is more promising. If the Reynolds number is controlled, the constant cross-sectional case has the highest Nu and h in the turn. If the mass flowrate is controlled, the accelerating case exhibits the lowest overall average Nu and h. The flow field results suggest that the secondary flow induced by the turn is weakened when the flow accelerates after the turn for the accelerating channel. The opposite is observed for the decelerating channel. The strength of the counterrotating vortex pair, turbulence level, and local heat transfer enhancements are closely correlated in a serpentine channel.
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      Heat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages

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    contributor authorWang, Hanlin
    contributor authorKlein, Denali
    contributor authorWright, Lesley M.
    date accessioned2025-04-21T10:35:01Z
    date available2025-04-21T10:35:01Z
    date copyright1/13/2025 12:00:00 AM
    date issued2025
    identifier issn0889-504X
    identifier otherturbo_147_8_081006.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306490
    description abstractThis study investigates the effect of acceleration and deceleration in the turn region of a two-pass, serpentine channel. Channel aspect ratios of 2:1 and 4:1 are considered in three combinations to investigate the effect of acceleration and deceleration through the turn region in a smooth, two-pass channel. For each aspect ratio combination, the experiments include Reynolds numbers ranging from 15,000 to 45,000 in the first passage and from 9,000 to 75,000 in the second pass. Surface heat transfer coefficient (h) distributions are measured by transient thermochromic liquid crystal technique, and the flow field characteristics are measured by tomographic PIV. Enhanced heat transfer on the side wall and downstream in the second pass is observed for all cases. Based on the first-pass Nusselt number (Nu) ratio, the accelerating case provides the best heat transfer enhancement. However, based on the second-pass Nu ratio, the decelerating case is more promising. If the Reynolds number is controlled, the constant cross-sectional case has the highest Nu and h in the turn. If the mass flowrate is controlled, the accelerating case exhibits the lowest overall average Nu and h. The flow field results suggest that the secondary flow induced by the turn is weakened when the flow accelerates after the turn for the accelerating channel. The opposite is observed for the decelerating channel. The strength of the counterrotating vortex pair, turbulence level, and local heat transfer enhancements are closely correlated in a serpentine channel.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleHeat Transfer and Flow Field Characteristics of Variable Aspect Ratio, Serpentine Passages
    typeJournal Paper
    journal volume147
    journal issue8
    journal titleJournal of Turbomachinery
    identifier doi10.1115/1.4067322
    journal fristpage81006-1
    journal lastpage81006-11
    page11
    treeJournal of Turbomachinery:;2025:;volume( 147 ):;issue: 008
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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