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Estimating the effective elastic modulus and specific fracture energy of snowpack layers from field experiments

Published online by Cambridge University Press:  25 July 2016

ALEC VAN HERWIJNEN*
Affiliation:
WSL Institute for Snow and Avalanche Research SLF, Davos, Switzerland
JOHAN GAUME
Affiliation:
WSL Institute for Snow and Avalanche Research SLF, Davos, Switzerland
EDWARD H. BAIR
Affiliation:
Earth Research Institute, University of California, Santa Barbara, CA, USA
BENJAMIN REUTER
Affiliation:
WSL Institute for Snow and Avalanche Research SLF, Davos, Switzerland
KARL W. BIRKELAND
Affiliation:
USDA Forest Service National Avalanche Center, Bozeman, MT, USA
JÜRG SCHWEIZER
Affiliation:
WSL Institute for Snow and Avalanche Research SLF, Davos, Switzerland
*
Correspondence: Alec van Herwijnen <vanherwijnen@slf.ch>
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Abstract

Measurements of the mechanical properties of snow are essential for improving our understanding and the prediction of snow failure and hence avalanche release. We performed fracture mechanical experiments in which a crack was initiated by a saw in a weak snow layer underlying cohesive snow slab layers. Using particle tracking velocimetry (PTV), the displacement field of the slab was determined and used to derive the mechanical energy of the system as a function of crack length. By fitting the estimates of mechanical energy to an analytical expression, we determined the slab effective elastic modulus and weak layer specific fracture energy for 80 different snowpack combinations, including persistent and nonpersistent weak snow layers. The effective elastic modulus of the slab ranged from 0.08 to 34 MPa and increased with mean slab density following a power-law relationship. The weak layer specific fracture energy ranged from 0.08 to 2.7 J m−2 and increased with overburden. While the values obtained for the effective elastic modulus of the slab agree with previously published low-frequency laboratory measurements over the entire density range, the values of the weak layer specific fracture energy are in some cases unrealistically high as they exceeded those of ice. We attribute this discrepancy to the fact that our linear elastic approach does not account for energy dissipation due to non-linear parts of the deformation in the slab and/or weak layer, which would undoubtedly decrease the amount of strain energy available for crack propagation.

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Papers
Creative Commons
Creative Common License - CCCreative Common License - BYCreative Common License - NCCreative Common License - ND
This is an Open Access article, distributed under the terms of the Creative Commons Attribution-NonCommercial-NoDerivatives licence (http://creativecommons.org/licenses/by-nc-nd/4.0/), which permits non-commercial re-use, distribution, and reproduction in any medium, provided the original work is unaltered and is properly cited. The written permission of Cambridge University Press must be obtained for commercial re-use or in order to create a derivative work.
Copyright
Copyright © The Author(s) 2016
Figure 0

Fig. 1. (a) Schematic representation of the experimental setup and coordinate system used in the analysis with x the slope parallel direction, y the slope normal direction and θ the slope angle. (b) FE model setup with a snow slab of total length L unsupported over the crack length r and rigidly supported at the base along the remaining length Lr. Triangles indicate fixed nodes.

Figure 1

Fig. 2. Post-processing to remove spurious displacement due to camera movement. (a) Slope parallel displacement with time before correction. Colors indicate the vertical position y0 of the markers relative to the weak layer. (b) Slope normal displacement with time before correction. Colors indicate the horizontal position x0 of the markers relative to the right edge of the PST. (c) Displacement field at r = rc before correction. The black dashed square shows the markers that were used to calculate the mean displacement used for correcting marker trajectories. (d), (e) and (f) displacements after correction.

Figure 2

Fig. 3. Ratio (dots) between numerically obtained mechanical energy $V_{\rm m}^{FEM} (r)$ and $V_{\rm m} (r)$ obtained with Eqn (2) for various input parameters. A ratio of one (black dashed line) would mean perfect agreement. (a) $V_{\rm m}^{FEM} (r)/V_{\rm m} (r)$ with elastic modulus E. (b) $V_{\rm m}^{FEM} (r)/V_{\rm m} (r)$ with density ρ. (c) $V_{\rm m}^{FEM} (r)/V_{\rm m} (r)$ with slope angle θ. (d) $V_{\rm m}^{FEM} (r)/V_{\rm m} (r)$ with the ratio between crack length r and slab thickness D. Colors indicate the crack length.

Figure 3

Fig. 4. (a) Ratio (dotted curves) between numerically obtained mechanical energy $V_{\rm m}^{FEM} (r)$ and $V_{\rm m} (r)$ obtained using Eqn (2) with slope angle θ. Colors indicate the ratio between crack length r and slab thickness D. (b) $V_{\rm m}^{FEM} (r)/V_{\rm m} (r)$ with r/D. Colors indicate θ. (c) Contour plot of $V_{\rm m}^{FEM} (r)/V_{\rm m} (r)$ with r/D and θ. The black dots represent the PST experiments.

Figure 4

Table 1. Overview of range of input parameters used in the FE simulations

Figure 5

Fig. 5. Displacement measurements for a PST performed on a weak layer consisting of rounding faceted particles with θ = 19°, D = 36 cm, $\rho _{slab} = 226\, {\rm kg} {\rm m}^{ - 3} $ and $r_{\rm c} = 20\, {\rm cm}$. (a) Negative slope parallel displacement with time. Colors indicate the vertical position |y0 | of the markers relative to the weak layer. (b) Slope normal displacement with time. Colors indicate the horizontal position x0 of the markers relative to the right edge of the PST. The insets represent a zoom of the bending phase before the onset of crack propagation. (c) Displacement field at r = rc. The direction of gravity is indicated with the arrow, which, for scale, is 20 cm long.

Figure 6

Fig. 6. Slope normal displacement uy with normalized distance x0/rc for all 222 tests (each color represent one test) at the critical cut length r = rc, i.e. the onset of crack propagation. The mean slope normal displacement of all experiments is depicted by the thick black curve.

Figure 7

Table 2. Overview of range of experimental parameters, effective elastic modulus of the slab $E^{\rm \star} $ and weak layer specific fracture energy wf. fps: frame rate of the recordings; θ: slope angle; ρ: average slab density; D: slope normal slab thickness; rc: mean critical cut length

Figure 8

Table 3. Percentage of tested weak layers by grain type, according to Fierz and others (2009)

Figure 9

Fig. 7. Derived mechanical energy with crack length r for the experiment shown in Figure 5. The red dots represent the key frames at which the saw cut length r was estimated from the images. The black line represents the best fit of $V_{\rm m}^* (r)$ (Eqn (7)) to the experimental data $V_{\rm m}^{{\rm PTV}} (r)$ (Eqn (6), blue dots), and the black dashed-dotted lines the 95% confidence interval. The green dashed line represents the tangent to the mechanical energy at $r = r_{\rm c} = 0.2\, {\rm m}$.

Figure 10

Fig. 8. Effective elastic modulus $E^{\rm \star} $ with slab density. Field data (blue dots) and power law fit (blue dashed curve). Also shown are the parameterizations from laboratory studies presented in Scapozza (2004) (green line), Camponovo and Schweizer (2001) (red line) and Sigrist (2006) (black line) as well as estimates from SMP measurements (squares) from Schweizer and others (2011).

Figure 11

Fig. 9. (a) Weak layer specific fracture energy by grain type. On each box, the central line is the median, the edges of the box are the 1st and 3rd quartiles, the whiskers extend to the most extreme data points. (b) Weak layer specific fracture energy vs total overlying stress σ0 = ρgD.

Figure 12

Fig. 10. (a) Uncertainty in the mean effective elastic modulus $E^{\rm \star} $ with mean measurement uncertainty at sites with more than one PST. The black line shows the one-to-one relation. Red dots show sites where the uncertainty in the mean was larger than 1.25 the mean measurement uncertainty. (b) Same as in (a) for the weak layer specific fracture energy wf.