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SOIL MECHANICS, ROCK MECHANICS AND UNDERGROUND STRUCTURES ANALYSIS ON MICROCOMPUTERS USING PLASTICITY THEORY: AN INTRODUCTION TO Z_SOIL.PC 2D/3D OUTLINE Short courses taught by A. Truty, K.Podles, Th. Zimmermann & coworkers in Lausanne, Switzerland August 27-28 2008 (1.5days),
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SOIL MECHANICS, ROCK MECHANICS AND UNDERGROUND STRUCTURES ANALYSIS ON MICROCOMPUTERS USING PLASTICITY THEORY: AN INTRODUCTION TO Z_SOIL.PC 2D/3D OUTLINE Short courses taught by A. Truty, K.Podles, Th. Zimmermann & coworkers in Lausanne, Switzerland August 27-28 2008 (1.5days), EVENT I: Z_SOIL.PC 2D course , at EPFL room CO121, 09:00 August 28-29 2008 (1.5days), EVENT II: Z_SOIL.PC 3D course , at EPFL room CO121, 14:00 participants need to bring their own computer: min 1GB RAM
LECTURE 1 • - Problem statement • Stability analysis • Load carrying capacity • Initial state analysis
PROBLEM COMPONENTS - EQUILIBRIUM OF 2-PHASE PARTIALLY SATURATED MEDIUM - NON TRIVIAL INITIAL STATE - NONLINEAR MATERIAL BEHAVIOR(elasticity is not applic.) - POSSIBLY GEOMETRICALLY NONLINEAR BEHAVIOR - TIME DEPENDENT -GEOMETRY -LOADS -BOUNDARY CONDITIONS
DISCRETIZATION IS NEEDED FOR NUMERICAL SOLUTION e.g. by finite elements Equilibrium on (dx ● dy)
12 +(12 /x2)dx2 f1 12 EQUILIBRIUM STATEMENT, 1-PHASE Domain Ω, with boundary conditions: -imposed displacements -surface loads and body forces: -gravity(usually) equilibrium 11 11+(11/x1)dx1 x2 x1 dx1 direction 1: (11/x1)dx1dx2+(12 /x2) dx1dx2+ f1dx1dx2=0 L(u)=ij/xj + fi=0, differential equation(sum on j)
SOLID(1-phase) BOUNDARY CONDITIONS 2.natural: on , 0 by default sliding fixed 1.essential: on d,
FORMAL DIFFERENTIAL PROBLEM STATEMENT Deformation(1-phase): (equilibrium) (displ.boundary cond.) (traction bound. cond.) Incremental elasto-plastic constitutive equation:
WHY elasto-PLASTICITY? • non coaxiality of stress • and strain increments 2.unloading elastic E plastic E sand
y E CONSTITUTIVE MODEL: ELASTIC-PERFECTLY PLASTIC 1- dimensional Remark: this problem is non-linear
y E CONSTITUTIVE MODEL: ELASTIC- PLASTIC With hardening(or softening) 1- dimensional hardening Eep H’ softening
NB: -softening will engender mesh dependence of the solution -some sort of regularization is needed in order to recover mesh objectivity -a charateristic length will be requested from the user when a plastic model with softening is used (M-W e.g.)
SURFACE FOUNDATION: FROM LOCAL TO GLOBAL NONLINEAR RESPONSE
F(x,t) REMARK The problems we tackle in geomechanics are always nonlinear, they require linearization, iterations, and convergence checks F 4.out of balance force after 1 iteration N(d),unknown Fn+1 6.Out of balance after 2 iterations <=>Tol.? 2.F Fn 5.linearized problem it.2 3.linearized problem it.1 1.Converged sol. at tn(Fn,dn) d d dn 1 dn+1
INITIAL STATE, STABILITYAND ULTIMATE LOAD ANALYSIS IN SINGLE PHASE MEDIA
BOUNDARY CONDITIONS (cut.inp) Single phase problem ( imposed, 0 by default) domain = +u u (u imposed)
WE MUST DEFINE: -GEOMETRY & BOUNDARY CONDITIONS -MATERIALS -LOADS -ALGORITHM
GEOMETRY & BOUNDARY CONDITIONS start by defining the geometry
Geometry with box-shaped boundary conditions
ALGORITHM: STABILITY DRIVER 2D Single phase
Assume STABILITY ALGORITHM with s then Algorithm: -set C’= C/SF tan ’=(tan )/SF -increase SF till instability occurs
ALTERNATIVE SAFETY FACTOR DEFINITIONS SF1: SF1= =m+s SF2: C’=C/SF2 tan’= tan/SF2 SF3: C’=C/SF3
ALGORITHM: STABILITY DRIVER ALTERNATIVE SAFETY FACTOR DEFINITIONS 2D Single phase
VISUALIZATION OF INSTABILITY Displacement intensities
LOCALISATION 1 Transition from distributed to localized strain
VALIDATION Slope stability 1984
ELIMINATION OF LOCAL INSTABILITY 1 SF=1.4- Material 2, stability disabled SF=1.4+ Slope_Stab_loc_Terrasse.inp
INITIAL STATE, STABILITY AND ULTIMATE LOAD ANALYSIS(foota.inp) IN SINGLE PHASE MEDIA
WE MUST DEFINE: -GEOMETRY & BOUNDARY CONDITIONS (+-as before) -MATERIALS( +-as before) -LOADS and load function -ALGORITHM
F(x,t) DRIVEN LOAD ON A SURFACE FOUNDATION Po(x) F=Po(x)*LF(t) LF t foota.inp
REMARK • It is often safer to use driven displacements to avoid • taking a numerical instability for a true failure, then: F=uo(x)*LF(t)
ALGORITHM: DRIVEN LOAD DRIVER axisymmetric analysis) =single phase
DRUCKER-PRAGER & MISES CRITERIA DRUCKER-PRAGER VON MISES Identification with Mohr-Coulomb requires size adjustment
3D YIELD CRITERIA ARE EXPRESSED IN TERMS OF STRESS INVARIANTS I1=tr= kk =3 = 11+22+33 ; 1st stress invariant J2=0.5 tr s**2=0.5 sij sji ; 2nd invariant of deviatoric stress tensor J3=(1/3)sij sjk ski ; 3rd invariant of deviatoric stress tensor
SIZE ADJUSTMENTS D-P vs M-C 3-dimensional,external apices 3-dimensional,internal apices Plane strain failure with (default) Axisymmetry intermediate adj. (default)
PLASTIC FLOW M-C(M-W) associated with D-P in deviatoric plane associated with D-P in deviatoric plane dilatant flow in meridional plane
SIGNS OF FAILURE: Localized displacements before at failure scales are different!