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Improved representation of laminar and turbulent sheet flow in subglacial drainage models

Published online by Cambridge University Press:  12 December 2023

Tim Hill*
Affiliation:
Department of Earth Sciences, Simon Fraser University, Burnaby, BC, Canada
Gwenn Elizabeth Flowers
Affiliation:
Department of Earth Sciences, Simon Fraser University, Burnaby, BC, Canada
Matthew James Hoffman
Affiliation:
Fluid Dynamics and Solid Mechanics Group, Los Alamos National Laboratory, Los Alamos, NM, USA
Derek Bingham
Affiliation:
Department of Statistics and Actuarial Science, Simon Fraser University, Burnaby, BC, Canada
Mauro Angelo Werder
Affiliation:
Laboratory of Hydraulics, Hydrology and Glaciology (VAW), ETH Zurich, Zurich, Switzerland Swiss Federal Institute for Forest, Snow and Landscape Research (WSL), Birmensdorf, Switzerland
*
Corresponding author: Tim Hill; Email: tim_hill_2@sfu.ca
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Abstract

Subglacial hydrology models struggle to reproduce seasonal drainage patterns that are consistent with observed subglacial water pressures and surface velocities. We modify the standard sheet-flow parameterization within a coupled sheet–channel subglacial drainage model to smoothly transition between laminar and turbulent flow based on the locally computed Reynolds number in a physically consistent way (the ‘transition’ model). We compare the transition model to standard laminar and turbulent models to assess the role of the sheet-flow parameterization in reconciling observed and modelled water pressures under idealized and realistic forcing. Relative to the turbulent model, the laminar and transition models improve seasonal simulations by increasing winter water pressure and producing a more prominent late-summer water pressure minimum. In contrast to the laminar model, the transition model remains consistent with its own internal assumptions across all flow regimes. Based on the internal consistency of the transition model and its improved performance relative to the standard turbulent model, we recommend its use for transient simulations of subglacial drainage.

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This is an Open Access article, distributed under the terms of the Creative Commons Attribution-NonCommercial-ShareAlike licence (http://creativecommons.org/licenses/by-nc-sa/4.0), which permits non-commercial re-use, distribution, and reproduction in any medium, provided the same Creative Commons licence is used to distribute the re-used or adapted article and the original article is properly cited. The written permission of Cambridge University Press must be obtained prior to any commercial use.
Copyright
Copyright © The Author(s), 2024. Published by Cambridge University Press on behalf of The International Glaciological Society
Figure 0

Table 1. Constants (top group) and model parameters (bottom group) for GlaDS simulations

Figure 1

Figure 1. Moody diagram, representing the friction factor $f_{\rm {D}} = \frac{h_{\rm {l}}}{\left({L\over D}\right){V^2\over 2g}}$ (for head loss $h_{\rm {l}}$ over a pipe of length L, diameter D, and with flow velocity V), as a function of the Reynolds number Re = VD/ν for different relative roughness scales ($\varepsilon$). The transition region (shaded grey, 1000 ≤ Re ≤ 3000) separates regions of laminar flow and turbulent flow. The laminar friction factor is $f_{\rm {D}} = \frac{64}{\rm {Re}}$ (Moody, 1944), and the friction factor in the transition and turbulent regimes is computed using the Colebrook–White equation (Colebrook and White, 1937).

Figure 2

Table 2. Summary of sheet-flow parameterizations with parameter values substituted in the general forms (Eqns. (1) and (2))

Figure 3

Figure 2. Scaled sheet thickness $\tilde h = {h}/{h_{\rm {crit}}}$ and scaled sheet discharge /ν for the five flux parameterizations in Table 2 and with a fixed hydraulic potential gradient. The sheet thickness is scaled by $h_{\rm {crit}}$, the sheet thickness that produces a Reynolds number equal to the transition threshold (ωRe = 1) for turbulent and laminar models.

Figure 4

Figure 3. Overview of synthetic model domain and moulin distribution. (a) Surface and bed elevation with moulins indicated by black circles. The bands at 15, 30, and 70 km indicate where model variables are aggregated in other figures. (b) Target moulin density (derived from Yang and Smith 2016) and density of randomly generated synthetic moulin design as a function of surface elevation.

Figure 5

Figure 4. Synthetic forcing scenario. Floatation fraction ${p_{\rm {w}}}/{p_{\rm {i}}}$ and channel discharge on 9 July (a-e) for turbulent 5/4 (a), turbulent 3/2 (b), laminar (c), transition 5/4 (d) and transition 3/2 (e) models, and width-averaged floatation fraction on 9 July (f). Width-averaged pressure in bands at x = 15 ± 2.5 km (g), x = 30 ± 2.5 km (h), and x = 70 ± 2.5 km (i) and imposed air temperature at 390 m a.s.l. used to force the temperature-index model (j). The centre of bands used for (g–i) are indicated by vertical lines in (a–f), and the time of (a–f) is shown by vertical lines in (g–i).

Figure 6

Table 3. Water pressure normalized by overburden (i.e., floatation fraction) for synthetic and KAN temperature-forcing scenarios. Winter floatation fraction is computed as the average value within x = 30 ± 2.5 km (Fig. 3) during the two months preceding the initial onset of surface melt. Summer floatation fraction is computed as the 95th-percentile width-averaged water pressure produced during the melt season within x = 30 ± 2.5 km. The bracketed number beside summer floatation fractions for the KAN scenario indicates the number of days water pressure exceeded overburden. Water pressure does not exceed overburden in the Synthetic scenario.

Figure 7

Figure 5. Turbulence index ωRe (log scale; a, b), transmissivity T (log scale; c, d), water depth h (log scale; e, f), potential gradient $\vert \nabla \phi \vert$ (linear scale; g, h), and effective turbulent conductivity (log scale; i, j) on 14 June (left column), and averaged for the band x = 30 ± 2.5 km (right column).

Figure 8

Figure 6. Reynolds number and channel discharge for synthetic scenario for turbulent 5/4 (a), turbulent 3/2 (b), laminar (c), transition 5/4 (d), and transition 3/2 (e) models.

Figure 9

Figure 7. Moody diagram computed from model outputs in the synthetic scenario for the five flux parameterizations (Table 2). The turbulent 3/2 model appears as a horizontal line since its friction factor is independent of Re and $\nabla \phi$. The results from the laminar model are displayed as a thick dashed line to distinguish the modelled results from the theoretical curves. The transition Reynolds number is shown as the solid black line at Re = 2000. For reference, the classical pipe-flow Moody diagram from Fig. 1 is shown in the background (thin black lines, right axis). Note that the scaling between the two axes is arbitrary.

Figure 10

Figure 8. KAN forcing scenario. Floatation fraction ${p_{\rm {w}}}/{p_{\rm {i}}}$ and channel discharge on 9 July (a–e) for turbulent 5/4 (a), turbulent 3/2 (b), laminar (c), transition 5/4 (d) and transition 3/2 (e) models, and width-averaged floatation fraction on 9 July (f). Width-averaged pressure in bands at x = 15 ± 2.5 km (g), x = 30 ± 2.5 km (h), and x = 70 ± 2.5 km (i) and imposed air temperature at 390 m a.s.l. used to drive the temperature-index model (black curve, right axis g–i). The centre of bands used for (g–i) are indicated by vertical lines in (a–f), and the time of (a–f) is shown by vertical lines in (g–i).

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