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Mesh Twisting Technique for Swirl Induced Laminar Flow Used to Determine a Desired Blade Shape

Mesh Twisting Technique for Swirl Induced Laminar Flow Used to Determine a Desired Blade Shape


Titill: Mesh Twisting Technique for Swirl Induced Laminar Flow Used to Determine a Desired Blade Shape
Höfundur: Helgadottir, Asdis   orcid.org/0000-0002-6653-1600
Lalot, Sylvain
Beaubert, Francois
Pálsson, Halldór   orcid.org/0000-0003-4112-6729
Útgáfa: 2018-10-10
Tungumál: Enska
Umfang: 1865
Háskóli/Stofnun: Háskóli Íslands
University of Iceland
Svið: Verkfræði- og náttúruvísindasvið (HÍ)
School of Engineering and Natural Sciences (UI)
Deild: Iðnaðarverkfræði-, vélaverkfræði- og tölvunarfræðideild (HÍ)
Faculty of Industrial Eng., Mechanical Eng. and Computer Science (UI)
Birtist í: Applied Sciences;8(10)
ISSN: 2076-3417
DOI: 10.3390/app8101865
Efnisorð: Swirling flow; Laminar flow; Mesh morphing; Guidance blades/vanes; OpenFOAM; Varmaflutningur; Vélaverkfræði
URI: https://hdl.handle.net/20.500.11815/1154

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Tilvitnun:

Helgadóttir, Á.; Lalot, S.; Beaubert, F.; Pálsson, H. Mesh Twisting Technique for Swirl Induced Laminar Flow Used to Determine a Desired Blade Shape. Appl. Sci. 2018, 8, 1865. doi:10.3390/app8101865

Útdráttur:

Swirling flow has been shown to increase heat transfer in heat exchangers. However, producing swirl while not presenting a severe pressure drop can be a challenge. In this paper, a desired shape of guidance blades for laminar swirl flow is determined by numerical simulation in OpenFOAM. Emphasis is on the mesh technique, where a predefined blade shape is formed by mesh twisting, or morphing. The validity of numerical simulations on a twisted mesh is shown by comparing it to the theoretical solution of laminar flow in a pipe without swirl and guidance blades. A sensitivity study shows that a cell size ratio of 0.025 of diameter is sufficient and affects the solution minimally. To determine the desired shape of guidance blades previously found optimal swirl decay and velocity profile for laminar swirling flow are utilized. Three blade shapes are explored: (I) with a twist angle that varies with axial location only; (II) having a deviation angle matching the theoretical deviation angle for laminar swirling flow; (III) same as II but with a hollow center. Simulations are performed for Re=100 and swirl number S=0.2. Case II is able to sustain swirl longest while maintaining a low pressure drop and is therefore a desired swirler shape profile as predicted theoretically.

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This is an open access article distributed under the Creative Commons Attribution License which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited (CC BY 4.0).

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