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Titel Failure-plane angle in Bentheim sandstone subjected to true triaxial stresses: experimental results and theoretical prediction
VerfasserIn Xiaodong Ma, John Rudnicki, Bezalel Haimson
Konferenz EGU General Assembly 2014
Medientyp Artikel
Sprache Englisch
Digitales Dokument PDF
Erschienen In: GRA - Volume 16 (2014)
Datensatznummer 250087742
Publikation (Nr.) Volltext-Dokument vorhandenEGU/EGU2014-1800.pdf
 
Zusammenfassung
We conducted true triaxial tests in the high-porosity (n = 24%), quartz-rich (95%), Bentheim sandstone. An important objective was to investigate the dependence of failure-plane angle θ (angle between the normal to the plane and Ïă1 direction) on the prevailing stress conditions. We employed two distinct loading paths, and seven Ïă3 magnitudes (between 0 and 150 MPa). In tests using the common loading path, Ïă2 and Ïă3 were fixed, while Ïă1 was raised monotonically to failure. In tests using the novel loading path (which facilitate comparison with theoretical predictions), Ïă3 was fixed, and the Lode angle, Θ (= tan-1 [(Ïă1 - 2Ïă2 + Ïă3) / 30.5(Ïă1 – Ïă3)]) was kept constant by raising Ïă1 and Ïă2 simultaneously at a set ratio b [= (Ïă2 -Ïă3)/(Ïă1 -Ïă3)] until failure occurred. Six stress ratios b (= 0, 1/6, 1/3, 1/2, 3/4, 1), i.e. six Θ (= tan-1 [(1-2b) / 30.5]) values from +π/6 (axisymmetric compression) to –π/6 (axisymmetric extension) were used. In axisymmetric common loading path tests, failure-plane angle θ generally declined as the applied Ïă3 = Ïă2 increased from about 80° at Ïă3 = Ïă2 = 0 MPa to 0° at Ïă3 = Ïă2 = 150 MPa (forming compaction bands). In tests where Ïă3 -‰  Ïă2, the resulting failure-plane strike was consistently parallel to Ïă2 direction. For low Ïă3, θ typically rose by up to 12° as Ïă2 rose from Ïă2 = Ïă3 to Ïă2 = Ïă1. However, the rise in θ with Ïă2 tended to diminish at higher Ïă3. A limiting case occurred at Ïă3 = 150 MPa, where failure plane remained at 0°, regardless of the rise in Ïă2. In the novel loading path tests, failure-plane angle θ declined monotonically for any given Lode angle Θ, from roughly 80° to 0°, as the mean stress at failure (Ïăoct,f) rose from about 20 MPa to around 220 MPa; for a constant Ïăoct,f, θ typically increased from 10° (at Ïăoct,f = 20 MPa) to 30° (at Ïăoct,f = 220 MPa) as Θ dropped from +π/6 (Ïă2 = Ïă3) to -π/6 (Ïă2 = Ïă1). We compared the measured θ with that predicted using equation 28 in Rudnicki (2013), an extension of the Rudnicki and Rice (1975) prediction to include the third stress invariant Θ. (Space does not permit detailing the equation in this abstract.) The theory treats octahedral shear stress at failure (τoct,f) and the resulting θ as dependent on Ïăoct,f and Θ. We used two series of the novel loading path tests: axisymmetric compression (Θ = +π/6) and pure shear (Θ = 0) to constrain that dependence. The failure conditions in the novel loading path tests were then simulated to compare the predicted failure-plane angles with the experimental results. The predictions were in general agreement with the experimental data, except when Θ = -π/6 (Ïă2 = Ïă1). In the common loading path tests, failure prediction replicated the general rise of the experimentally observed θ with Ïă2 for a given Ïă3,as well as the diminished rise at high Ïă3 magnitudes. The reasonable agreement between the predicted and the observed failure-plane angle demonstrated the applicability and the limitations of Rudnicki’s (2013) theory.