Heat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various ShapesSource: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007::page 71011-1DOI: 10.1115/1.4056775Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Additive manufacturing (AM) provides the ability to fabricate highly customized internal cooling passages that are relevant to gas turbine components. This experimental study examines the pressure loss and heat transfer performance of a range of fundamental channel shapes that were produced using direct metal laser sintering. Circular, hexagonal, pentagonal, elliptical, diamond, square, rectangular, trapezoidal, and triangular channel cross sections were investigated. To maintain the same convective surface area between shapes, the wetted perimeters of the channel cross sections were kept constant. Parallel computational fluid dynamic simulations were performed to understand the relationships in cooling performance between several channel shapes. Several characteristic length scales were evaluated to scale the pressure loss and heat transfer measurements. Among the channel shapes investigated, the diamond channel showed the lowest Nusselt number and friction factor. The pentagon exhibited a similar Nusselt number as the circular channel despite having a lower friction factor. There was no difference in scaling the friction factor or Nusselt number results of the different channel shapes between using the square root of cross-sectional area compared to hydraulic diameter as the characteristic length scale
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contributor author | Wildgoose, Alexander J. | |
contributor author | Thole, Karen A. | |
date accessioned | 2023-08-16T18:11:30Z | |
date available | 2023-08-16T18:11:30Z | |
date copyright | 2/10/2023 12:00:00 AM | |
date issued | 2023 | |
identifier issn | 0889-504X | |
identifier other | turbo_145_7_071011.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4291588 | |
description abstract | Additive manufacturing (AM) provides the ability to fabricate highly customized internal cooling passages that are relevant to gas turbine components. This experimental study examines the pressure loss and heat transfer performance of a range of fundamental channel shapes that were produced using direct metal laser sintering. Circular, hexagonal, pentagonal, elliptical, diamond, square, rectangular, trapezoidal, and triangular channel cross sections were investigated. To maintain the same convective surface area between shapes, the wetted perimeters of the channel cross sections were kept constant. Parallel computational fluid dynamic simulations were performed to understand the relationships in cooling performance between several channel shapes. Several characteristic length scales were evaluated to scale the pressure loss and heat transfer measurements. Among the channel shapes investigated, the diamond channel showed the lowest Nusselt number and friction factor. The pentagon exhibited a similar Nusselt number as the circular channel despite having a lower friction factor. There was no difference in scaling the friction factor or Nusselt number results of the different channel shapes between using the square root of cross-sectional area compared to hydraulic diameter as the characteristic length scale | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Heat Transfer and Pressure Loss of Additively Manufactured Internal Cooling Channels With Various Shapes | |
type | Journal Paper | |
journal volume | 145 | |
journal issue | 7 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4056775 | |
journal fristpage | 71011-1 | |
journal lastpage | 71011-11 | |
page | 11 | |
tree | Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007 | |
contenttype | Fulltext |