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A fully three-dimensional finite-element model applied to velocities on Storglaciären, Sweden

Published online by Cambridge University Press:  20 January 2017

Brian Hanson*
Affiliation:
Center for Climatic Research, Department of Geography, University of Delaware, Newark, Delaware 19716, U.S.A.
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Abstract

A finite-element model that solves the stress-balance equations for glacier dynamics in three dimensions has been developed by extending previous flow-plane models. This model retains all terms of the stress tensor and uses a Glen-type power law for viscosity calculations. In the paper, the model is applied to Storglaciären, Sweden, to explore both the glacier’s dynamics and the model’s characteristics. Values of the stiffness parameter B of 0.20–0.22 MPa year1/n were required to match observed strain rates on Storglaciären. Overall velocities required imposition of a problematically small sliding speed. Stress fields implied by the model simulation showed that the glacier receives its largest driving force from a high-slope zone near the equilibrium line, and that a large proportion of the resistive stress comes from lateral drag. Lateral drag is enhanced on this glacier by being frozen to its sidewalls and by a turning of the main flow as it comes out of the main, or northern, cirque.

Information

Type
Research Article
Copyright
Copyright © International Glaciological Society 1995
Figure 0

Fig. 1.Model element grids and coordinates for Storglaciären simulations, a. Horizontal grid with x (east) and y (north) coordinates. Circles connected with the dotted line indicate the chain of nodes used as an approximate central flowline for cross-section diagrams. Solid diamonds indicate positions of three boreholes for which deformation measurements were available, b. Vertical grid with z (altitude) and path length along the approximate flowline.

Figure 1

Fig. 2.Scatter plot of agreement between horizontal velocities in the control simulation and Storastaknet observations, including a perfect-correspondence line. Horizontal speeds are indicated with ο, x components with * and y components with +. All speeds are in m year−1.

Figure 2

Fig. 3.Simulated and observed horizontal speeds at locations of three boreholes. Dashed lines are observations and solid lines are the control simulation.

Figure 3

Fig. 4.Map of observed Storastaknet surface velocities and corresponding values from the control run. Dots indicate the base of each vector. Solid lines are model simulation and dashed lines are observations.

Figure 4

Table 1.Model evaluation statistics describing the fit between 32 Storastaknet surface velocities and closely corresponding surface nodal points of the control run. All quantities are in m year−1, except than the index of agreement is dimensionless. r.m.s.e. indicates root mean-squared error

Figure 5

Table 2.Summary of all model runs discussed in the text. The first three numerical columns indicate the applied conditions of stiffness (MPa year1/n), sliding-speed parameter (103m year−1 MPa−2) and water-head fraction. Fit to Storastaknet data is indicated by the vector correlation (ρ), regression-scale factor (β), turning angle (θ, counterclockwise) and magnitude of regression “intercept” (α, m year−1). Velocities averaged over the entire model domain, its surface and its-base are given as average horizontal and vertical in m year−1

Figure 6

Fig. 5.Control velocity simulation, a. Horizontal surface vectors, b. Horizontal base vectors, c. Vertical vectors. 5 × vertical exaggeration. Every other node in each vertical column was omitted for clarity.

Figure 7

Fig. 6.Horizontal speeds along the approximate flowline using three different values of the stiffness parameter B. Lower solid curve is the basal speed applied in all three cases. Upper curves are surface speeds for control run (solid curve. Β = 0.20 MPa year1/n), increased stiffness (short dashes. Β = 0.22 M Pa year1/n), and decreased stiffness (long dashes, Β = 0.18 MPa year1/n).

Figure 8

Fig. 7.Horizontal speeds along the approximate flowline using four different values of the roughness parameter C. Lower curves are sliding speeds and upper curves are surface speeds. The four cases are no sliding (c = 0, dot dashed curve), increased friction (c = 5 × 103 m year −1 MPa−2, long dashes), control (c =10 × 103 m year−1 MPa−2. solid curve), and decreased friction (c =20 × 103 m year−1 MPa−2, short dashes).

Figure 9

Fig. 8.Horizontal speeds along the approximate flowline using four different assumptions about internal water pressure. Lower curves are sliding speeds and upper curves are surface speeds. Cases are control (variable b, solid curve), constant low water (b = 0.3, long dashes), constant medium water (b = 0.5, short dashes), and constant high water (b = 0.7, dot-dashed).

Figure 10

Fig. 9.Horizontal speeds along the approximate flowline using five different values of the flow-law exponent n. Control-run values of base and surface velocity are shown as solid lines. Dashed lines are surface velocities, labeled With their respective values of n.

Figure 11

Fig. 10.Vectors of driving stress (, solid lines) and basal resistance (, dotted lines). Dots represent center points of basal elements and are the bases of the vectors. Basal resistances have reversed direction for easier comparison to the driving forces (see discussion in text).

Figure 12

Fig. 11.Vertically integrated stress components in each element column. All values in the smith cirque were small, so they have been mostly eliminated to aid in graphical clarity. Dimensions are M Pam, or M Nm−1.