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Water-pressure Coupling of Sliding and Bed Deformation: II. Velocity-Depth Profiles

Published online by Cambridge University Press:  20 January 2017

R.B. Alley*
Affiliation:
Geophysical and Polar Research Center, University of Wisconsin–Madison, Madison, Wisconsin 53706–1692, U.S.A.
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Abstract

Basal motion of a glacier resting on an unconsolidated bed can arise from sliding between ice and bed, ploughing of clasts through the upper layer of the bed, pervasive deformation of the bed, or shearing across discrete planes in the bed. Theoretical analyses and limited observations of soft-bedded glaciers not dominated by supply of channelized melt water from the surface suggest that sliding will be slow if the bed contains abundant clasts in the 1–10 mm size range, and that high velocities by ploughing are unlikely though possible. Pervasive deformation usually will account for 60–100% of the basal velocity, and the strain-rate will be proportional to the basal shear stress and inversely proportional to the square or cube of the effective pressure. These hypotheses are based on results of part I in this series, and allow modeling of Ice Stream B, West Antarctica, in part III of this series.

Information

Type
Research Article
Copyright
Copyright © International Glaciological Society 1989
Figure 0

Fig. 1. Coordinate axes for till-deformation calculations, with the origin at the ice-till inter face (or the top of the till if there is a significant water layer), z positive downward, and x positive in the direction of flow. The ice velocity is ui, the sliding velocity is uy the till velocity is u, the till velocity at z = 0 is u0, and ui = us + U0 if there is no ice deformation. The pervasively deforming till thickness is Z1.

Figure 1

Table I. Equations for velocity-depth profiles in till with a = 1

Figure 2

Table 2. Equations for average velocity in till with a = 1

Figure 3

Fig. 3. Depth-averaged velocity of pervasive deformation, u, normalized by u0, plotted against x (= chi), for different values of x (ω= omega); all variables are defined in the caption to Figure 2. Each plot contains curves for b = 0, 1, 2, 3, and 5 (indicated to the lower right of the appropriate curve) assuming a = 1. The average velocity (and thus till flux) decreases with increasing b and ω and with decreasing x. The likely values of x, b, and ω discussed in this paper and in part III give u/u ≈ 0.1–0.5.

Figure 4

Fig. 2. Velocity-depth plots. Plots of u/u0 (horizontal till velocity normalized by velocity at top of till) are shown against relative depth, ψ (= psi = z/z1 where Z1 is the base of pervasive deformation and z is the depth). The exponent a = 1 in equation (24), and each column of plots is headed by the value of the exponent b used in that column; each row uses the value of ω shown at the left (ω = omega = Z1Zzv where z2 is the depth at which the shear stress would equal the strength of the pervasively deforming till). Each plot contains curves for x = 0.01, I, 10, 100, where x = Z0/z1 and z0 is the depth at which the effective pressure, N, in the till is twice the value at the ice-till interface, N0. Curves for b = 0 are independent of x as shown. For b ≥ 1, curves are identified by x values placed to their lower right, unless otherwise indicated. The limiting case of x = 0, b > 0 gives a curve plotting on the top and left coordinate axes (as does b →∞); the x = 0.01 curves for b = 5 are close to this behavior. In the limit of x → ∞, curves with b ≠ O become identical to the b = 0 curves; the x = 10 and x = 100 curves for small b are essentially at this limit and plot quite close together. All curves are monotonie and smooth; slight irregularities in the figure arise from the computerized plotting package used.

Figure 5

Fig. 4. Measured velocity-depth profiles of till beneath Breidamerkurjökull (Boulton and Hindmarsh, 1987, fig. 2) plotted on the scale defined in the caption to Figure 2, Numbers 1–4 refer to the arrays 1–4 shown in Figure 2 of Boulton and Hindmarsh (1987). The inflection points that I identify with the base of pervasive deformation are indicated by arrows.

Figure 6

Fig. 5. Curves from Figure 4 above the inflection points, recalculated so that u = 0, ψ = 1 at the inflection points. The curve labeled “model” is calculated from equation (28) with a = 1, b = 2, x=7, and ω = 0.9.