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Relating crevassing to non-linear strain in the floating part of Jakobshavn Isbræ, West Greenland

Published online by Cambridge University Press:  14 September 2017

Paul R. Prescott
Affiliation:
Department of Spatial Information, Science, and Engineering, University of Maine, Orono, ME 04469-5790, U.S.A.Institute for Quaternary and Climate Studies, Bryand Global Science Center, University of Maine, Orono, ME 04469-5790, U.S.A. E-mail: terry.hughes@maine.edu
James P. Kenneally
Affiliation:
Department of Physics, University of Maine, Orono, ME 04469-5790, U.S.A.
Terence J. Hughes
Affiliation:
Department of Geological Sciences, University of Maine, Orono, ME 04469-5790, U.S.A.Institute for Quaternary and Climate Studies, Bryand Global Science Center, University of Maine, Orono, ME 04469-5790, U.S.A. E-mail: terry.hughes@maine.edu
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Abstract

Jakobshavn Isbræ is a major ice stream that drains the west-central Greenland ice sheet and becomes afloat in Jakobshavn Isfjord (69° N, 49° W), where it has maintained the world’s fastest-known sustained velocity and calving rate (7 kma−1) for at least four decades. The floating portion is approximately 12 km long and 6 km wide. Surface elevations and motion vectors were determined photogrammetrically for about 500 crevasses on the floating ice, and adjacent grounded ice, using aerial photographs obtained 2 weeks apart in July l985. Surface strain rates were computed from a mesh of 399 quadrilateral elements having velocity measurements at each corner. It is shown that heavy crevassing of floating ice invalidates the assumptions of linear strain theory that (i) surface strain in the floating ice is homogeneous in both space and time, (ii) the squares and products of strain components are nil, and (iii) first- and second-order rotation components are small compared to strain components. Therefore, strain rates and rotation rates were also computed using non-linear strain theory. The percentage difference between computed linear and non-linear second invariants of strain rate per element were greatest (mostly in the range 40–70%) where crevassing is greatest. Isopleths of strain rate parallel and transverse to flow and elevation isopleths relate crevassing to known and inferred pinning points.

Information

Type
Research Article
Copyright
Copyright © International Glaciological Society 2003
Figure 0

Fig. 1.jakobshavn isbr×floating injakobshavn isfjord at 69° n, 49° w,west greenland. photo flight on 24 july 1985 by henderson aerial surveys, inc. surface elevations were contoured at 2 m intervals by kucera international.

Figure 1

Fig. 2.Thinning retreat of Jakobshavn Isbræ since the Little based Age in Greenland. Top: ice surface elevations in 1850 (?) 19 95). on the upper limit of glacially polished bedrock (Prescott, Bottom: retreat of the calving front, 1850–1964 (Carbonnell and Bauer, 1968).

Figure 2

Fig. 3.Surface elevations on Jakobshavn Isbræ contoured at 5 m intervals above the OSU91A1F geoid (Prescott, 19 line is the tentative grounding line. The long rectangle encloses crevasses in the Zipper.

Figure 3

Fig. 4.Surface velocity vectors of floating and grounded ice at the head of jakobshavn isfjord (prescott, 19 95). velocities range over three orders of magnitude, so slow velocities are only points inside arrowheads.

Figure 4

Fig. 5.Isopleths of surface velocities contoured at 0.5 km a–1 intervals at the head of jakobshavn isfjord (Prescott, 1995).

Figure 5

Fig. 6.A mesh of quadrilateral elements created from point locations on Jakobshavn Isbr×. Top: the complete mesh. Bottom: the part of the mesh inside the bold border showing the percentage difference between computed linear and non-linear strain rates for each element.

Figure 6

Fig. 7.Non-linear principal strain rates computed for each element of the mesh generated from point measurements of surface velocity on Jakobshavn Isbræ (Prescott, 1995).

Figure 7

Fig. 8.Isopleths contoured at 0.1 a–1intervals for non-linear strain rates (top) and (bottom) respectively parallel transverse to ice-flow vectors in Figure 4. Also shown is the portion of the finite-element mesh in Figure 5 that was used calculations.