Transient simulation of an atmospheric boundary layer flow past a heliostat using the Scale-Adaptive Simulation turbulence model

dc.contributor.authorPoulain, P.E.
dc.contributor.authorCraig, K.J. (Kenneth)
dc.contributor.authorMeyer, Josua P.
dc.contributor.emailken.craig@up.ac.zaen_US
dc.date.accessioned2022-07-13T10:59:06Z
dc.date.available2022-07-13T10:59:06Z
dc.date.issued2021-11
dc.description.abstractHeliostat fields are exposed to changing climatic conditions as they are mostly erected in open environments where the wind naturally features a high unsteadiness at low altitude due to the ground effects. Much of the computational fluid dynamics (CFD) content in the open literature is focused on Reynolds–averaged-Navier–Stokes (RANS) simulations, which can only predict mean loads. This paper considers an isolated heliostat in worst-case orientation. The drag force is numerically modelled by means of a Scale-Resolving Simulation (SRS) in ANSYS v19. This paper firstly deals with two different methods that generate perturbations at the inlet boundary: the spectral synthesiser and the vortex method. In an empty domain, an atmospheric boundary layer (ABL) profile is modelled based on a wind tunnel experiment. Secondly, the wind tunnel test of a single heliostat model in upright orientation is replicated, aiming to model the mean and peak drag forces. Applicable for highly separated flows, the Scale-Adaptive Simulation (SAS) turbulence model is employed as it is computationally more affordable than a Detached Eddy Simulation (DES) approach. The latter would require a higher grid resolution and a reduced time step size. The SAS showed little but acceptable decay of the inlet profiles whilst achieving lateral homogeneity. The mean and root-mean-square error of the drag force signal showed a deviation with the experiment of 0.04% and 5.8%, respectively, whereas the error on the peak drag forces was around 18%, possibly mostly due to the under-prediction of the turbulent integral length scale at the model location.en_US
dc.description.departmentMechanical and Aeronautical Engineeringen_US
dc.description.librarianhj2022en_US
dc.description.sponsorshipThe University of Pretoria, South Africa and the South African National Research Foundation.en_US
dc.description.urihttp://www.elsevier.com/locate/jweiaen_US
dc.identifier.citationPoulain, P., Craig, K.J. & Meyer, J.P. 2021, 'Transient simulation of an atmospheric boundary layer flow past a heliostat using the Scale-Adaptive Simulation turbulence model', Journal of Wind Engineering and Industrial Aerodynamics, vol. 218, art. 104740, pp. 1-14, doi : 10.1016/j.jweia.2021.104740.en_US
dc.identifier.issn0167-6105
dc.identifier.other10.1016/j.jweia.2021.104740
dc.identifier.urihttps://repository.up.ac.za/handle/2263/86138
dc.language.isoenen_US
dc.publisherElsevieren_US
dc.rights© 2021 Elsevier Ltd. All rights reserved. Notice : this is the author’s version of a work that was accepted for publication in Journal of Wind Engineering and Industrial Aerodynamics. Changes resulting from the publishing process, such as peer review, editing, corrections, structural formatting, and other quality control mechanisms may not be reflected in this document. A definitive version was subsequently published in Journal of Wind Engineering and Industrial Aerodynamics, vol. 218, art. 104740, pp. 1-14, 2021. doi : 10.1016/j.jweia.2021.104740.en_US
dc.subjectComputational fluid dynamics (CFD)en_US
dc.subjectScale-adaptive simulation (SAS)en_US
dc.subjectAtmospheric boundary layer (ABL)en_US
dc.subjectHeliostaten_US
dc.subjectTurbulence power spectrumen_US
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dc.titleTransient simulation of an atmospheric boundary layer flow past a heliostat using the Scale-Adaptive Simulation turbulence modelen_US
dc.typePreprint Articleen_US

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