A Damage Constitutive Model for a Rock under Compression after Freeze-Thaw Cycles Based on the Micromechanics
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Hindawi Geofluids Volume 2021, Article ID 3177464, 11 pages https://doi.org/10.1155/2021/3177464 Research Article A Damage Constitutive Model for a Rock under Compression after Freeze-Thaw Cycles Based on the Micromechanics Hongyan Liu ,1,2 Xiaochen Zhang ,3 and Xidong Yan 4 1 College of Engineering & Technology, China University of Geosciences (Beijing), Beijing 100083, China 2 Key Laboratory of Deep Geodrilling Technology of Ministry of Natural Resources, Beijing 100083, China 3 School of Safety Engineering, North China Institute of Science and Technology, Beijing 101601, China 4 RIOH Transport Consultants Ltd, Beijing 100088, China Correspondence should be addressed to Hongyan Liu; lhyan1204@126.com Received 12 May 2021; Accepted 8 July 2021; Published 23 July 2021 Academic Editor: Yu Wang Copyright © 2021 Hongyan Liu et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited. The freeze-thaw cycles will cause continuous damage to the rock, which is much related to the microcrack length, rock permeability, and frost heaving pressure. However, the failure mechanism of the rock under compression after freeze-thaw cycles is not very clear; therefore, it is studied with the damage theory here. First of all, according to the hydraulic pressure theory, the relationship between the frost heaving pressure and the microcrack propagation length in one single microcrack is established based on the elastoplastic mechanics and fracture theory. Second, by assuming the total strain of the rock under compression is comprised of the initial damage strain, elastic strain, additional damage strain, and plastic damage strain, a constitutive model for a rock based on the deformation and propagation of the microcrack under compression after freeze-thaw cycles is established. Finally, the proposed model is verified with the test result. In all, the proposed model can perfectly reflect the deterioration of the rock mechanical behavior under compression after the freeze-thaw cycles. 1. Introduction deteriorate and degrade to some degree in terms of the com- pressive strength, elastic modulus, mass density, and so on. Rock deterioration under freeze-thaw cycles is a hot issue in No, many research works have been done in this field. many engineering projects in cold regions. This deterioration Neaupane and Yamabeb [9] proposed a nonlinear elastoplas- proceeds with the freeze-thaw cycles, and the rock will grad- tic constitutive relationship and a two-dimensional (plane ually lose its stiffness and strength. stress) numerical modeling on the basis of the finite element Water in the microcrack is assumed to be the key factor method. With the continuum mechanics, Exadaktylos [10] leading to the rock deterioration under freeze-thaw cycles. established a coupled model for the saturated porous rocks The deterioration mechanism of the porous media under under freeze-thaw cycles which can be used for analyzing freeze-thaw cycles was firstly described by Powers [1]. the preliminary thawing experiments on the porous sand- According to his theory, the frost heaving pressure will be stone. According to the freeze-thaw cyclic fatigue tests on generated by 9% volume expansion when water in the closed sandstone and shale, Tang et al. [8] assumed that the rock microcrack freezes into ice. It will make the microcrack prop- damage process included two coupled parts, e.g., the damage agate and cause damage to the rock. Thereafter, lots of labo- induced by the freeze-thaw cycles and the damage evolution ratory tests have been done by many researchers, for caused by stress erosion. And then, a frost damage constitu- instance, Altindag et al. [2], Momeni et al. [3], Nicholson tive model is accordingly established. Based on the mass con- and Nicholson [4], Zhang et al. [5], Wang et al. [6], Tounsi servation law, energy conservation law, and the principle of et al. [7], and Tang et al. [8]. All these results indicated that static equilibrium, Kang et al. [11] studied the thermo- with the increasing number of freeze-thaw cycles, rock will hydro-mechanical coupling mechanism and then proposed
2 Geofluids a new THM (thermo-hydro-mechanical) coupling model by y considering phase change effect, in which the water migra- Δb tion caused by segregation potential and temperature gradi- ent is described. By considering the coupling effects among x p 2b fluid flow, heat transfer, crystallization, and deformation in porous media, Wu et al. [12] established a thermo-hydro- 2a Δa ry salt-mechanical coupled model for fully saturated porous Δa' media with phase change. From the viewpoint of the energy conservation law, mass conservation law, and the principle Figure 1: The microcrack propagation model under the frost of static equilibrium considering water/ice phase change, heaving pressure. 2a and 2b are the length and width of the Huang et al. [13] set up a fully coupled THM model and ver- microcrack, respectively. △a and △b are the propagation length of ified its validity with the laboratory test. Based on a the microcrack along two directions, respectively. r y is the length microstructure-based random finite element model for the of the plastic zone near the microcrack tip. △a ′ is the equivalent frozen soil, Dong and Yu [14] established a holistic model propagation length of the microcrack. to simulate the temperature, stress, and deformation in fro- zen soil and implement a model to simulate frost heave and heaving pressure will lead to the rock damage. When freez- stress on water pipelines. In order to consider the migration ing, the frost heaving pressure p acts on the inner wall of of unfrozen water during freezing, Wang et al. [15] proposed the microcrack normally and evenly. a general thermo-mechanical-water migration coupled con- The following assumptions are made in this study: (1) the stitutive model to model mechanical degradation of rocks microcrack is always elliptical during the whole freeze-thaw subjected to freeze-thaw cycles. Fan et al. [16] established a cycles. That is to say, the shape of the microcrack is the same; universal damage constitutive model under freeze-thaw and only its size changes; (2) the rock particle is assumed to be loading conditions based on the statistical damage constitu- unchanged; (3) the microcrack is always saturated, and the tive model. Meanwhile, it can be seen that plasticity theory microcrack propagation obeys the linear elastic fracture [17, 18] is often adopted to describe the nonlinear mechani- mechanics; and (4) the propagation process of the micro- cal behavior of rock-like materials under freeze-thaw cycles. crack is stable. Rock properties including the microcrack size distribu- Water will change into ice with the volume expansion tion and permeability also have significant influence on rock when temperature decreases to a certain degree. But because mass mechanical behavior [19–22]. Hori and Moriniro [23] of the constraint of the microcrack wall, the stress induced by treated the shape of the microcrack as an ellipse in rock the ice volume expansion will act on the microcrack inner and set up a micromechanical model for the microscopic wall which will produce the elastic strain energy in the rock. process. Although they assumed that the rock damage was When the stress intensity factor K I is larger than the rock induced by the microcrack propagation due to the water fracture toughness K IC , the microcrack will propagate, which freezing and movement, they did not discuss the influence will lead to the release of the elastic strain energy. According of microcrack distribution and permeability on rock deterio- to the Griffith energy balance theory, there is ration. Therefore, the main objective of this research is to present an elastoplastic damage model for the rock with ran- W = E − U, ð1Þ dom distribution of the microcrack and the plastic yield cri- terion of the homogeneous medium combined with the where W, E, are U are work done by the frost heaving pres- micromechanical damage model to simulate the rock plastic sure, elastic strain energy stored in the rock, and the reduced deformation. The total strain of the rock is assumed to be total potential energy of the whole system, respectively. comprised of initial damage strain, elastic strain, additional Assume the elastic strain energy releases completely dur- damage strain, and plastic damage strain [24], where the ini- ing the microcrack propagation, Equation (1) can be written tial damage strain caused by the freeze-thaw cycles is calcu- into lated by the initial compliance matrix which is the function of freeze-thaw cycles. Meanwhile, the Drucker-Prager crite- W = −U: ð2Þ rion is adopted to describe the plastic behavior of rock under compression, in which the microcrack radius is assumed to The work W done by the frost heaving pressure on the obey an exponential law [25]. Finally, the validity of the pro- inner wall of the microcrack is expressed as posed model is verified with the experiment results. W = 2 × ðp × 2a × ΔbÞ = 4paΔb, ð3Þ 2. Propagation of One Single Microcrack under Frost Heaving Pressure where p is the frost heaving pressure, △b is the microcrack 2.1. The Relationship between the Microcrack Propagation opening displacement increment, shown in Figure 1. Length and Ice Pressure in One Single Microcrack. Figure 1 The reduced total potential energy U of the whole system illustrates a two-dimensional propagation model for one sin- in Equation (2) can be expressed as gle microcrack under the frost heaving pressure. The micro- crack is an ellipse, and its propagation under the frost U = −2G × Δa, ð4Þ
Geofluids 3 where △a is the microcrack propagation length and G is the For the rock especially the soft rock, the plastic zone will microcrack Griffith energy release rate. be formed near the microcrack tip when the microcrack wall There is a relationship between the volume of water and is loaded by the frost heaving pressure. So, in order to satisfy that of the ice [26]. Without considering the constraint of the requirement of the linear elastic fracture mechanics, it is the microcrack wall, we assume the ice expansion volume is necessary to deal with the plastic zone near the microcrack △V i under the free condition. However, in practice, the ice tip with the equivalent method. The plastic region reduces is loaded by the stress p, and accordingly, the corresponding the stiffness of the rock which is equivalent to a longer micro- volumetric strain εv can be calculated: crack. The equivalent propagation length a ′ of the micro- crack is [27] 3ð1 − 2νi Þ εv = p, ð5Þ Ei a ′ = a + ry , ð10Þ where Ei and vi are the ice elastic modulus and Poisson’s ratio, and here, they are assumed to be 600 MPa and 0.3, respectively. where a is the original microcrack length and ry is the Then, the actual volume increment ΔV i′ is length of the plastic zone near the microcrack tip shown in Figure 1, which can be expressed as for a plane stress ΔV i′ = ΔV i − V i ε, ð6Þ issue [27]. where V i is the volume of water before freezing. According to the relationship of the water volume before 1 KI 2 ry = , ð11Þ and after the phase change, there is 2π σs πab + ΔV i′ = πða + ΔaÞðb + ΔbÞ: ð7Þ where σs is the rock yield strength and K I is the first stress The microcrack propagation length can be obtained by intensity factor at the microcrack tip. combining Equations(3), (4), (6), and (7) So after amendment, the actual propagation length Δa ′ of the microcrack shown in Figure 1 is AðΔaÞ2 + BðΔaÞ + C = 0, ð8Þ Δa ′ = Δa + r y : ð12Þ where A = πG, B = πð2pab + aGÞ, and C = −2ΔV i′pa. Solving Equation (8) yields qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi The shape of the microcrack after propagation is shown −ð2abp + aGÞπ + ð2abp + aGÞ2 π2 + 8Gpa × ΔV i′ as the dotted line in Figure 1. Δa = : After m freeze-thaw cycles, the microcrack half-length 2Gπ ð9Þ am is qffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi −ð2am−1 bp + am−1 GÞπ + ð2am−1 bp + am−1 GÞ2 π2 + 8Gpam−1 × ΔV i′ am = am−1 + : ð13Þ 2Gπ The microcrack propagation corresponds to the rock where the characteristic time τ is [28] damage, and accordingly, the rock elastic modulus and com- pressive strength will also decrease. 8 1−ν gavL τ= Rf , ð15Þ 3π μ v2s 2.2. The Frost Heaving Pressure. According to Walder and Hallet [28], the frost heaving pressure pi is related to the duration time of the low temperature, the value of tempera- where pi ðtÞ is the frost heaving pressure of ice at time t; Lð ture, the volume of ice and water, and flow resistance, which −T c Þ/vs T a = 1:1 MPa/° C × ð−T c Þ. Lð−T c Þ is the fusion heat can be calculated by of ice at T = T c , kJ/mol; vs and vL are the relative volume of ice and water, respectively; when T < −1°C, vL = 0:07 and vs = 0:93 [29]; T a is the absolute temperature, 273.15 K; p0 is Lð−T c Þ p i ðt Þ = 1 − e−ðt/τÞ + p0 e−ðt/τÞ , ð14Þ the initial frost heaving pressure, and according to the exper- vs T a iment result, it is 2 MPa; v is the rock Poisson ratio; μ is the
4 Geofluids 24 age strain, elastic strain, plastic strain, and additional damage strain induced by the microcrack propagation. It can be 20 expressed as 16 ε = εd + εe + εda + εp , ð17Þ p (MPa) 12 8 where ε is the total strain, εd is the initial damage strain, εe is the elastic strain, εda is the additional damage strain, and εp is 4 the plastic strain. Their calculation methods are discussed below. 0 0 2 4 6 8 10 12 3.2.1. Initial Damage Strain Induced by Freeze-Thaw Cycles. t (h) The initial damage strain induced by freeze-thaw cycles is Figure 2: Variation of the frost heaving pressure with time during ½εd = ½Cd ½σ, ð18Þ one freeze-thaw cycle. where ½Cd is the initial damage compliance matrix. rock shear modulus, MPa; Rf is the flow resistance, Pa·s/m; g Assume the half-length of the ith microcrack becomes am is the gravitational acceleration, m/s2; a is the microcrack after m freeze-thaw cycles. αi is the orientation of the ith half-length. Here, the freezing and thawing temperatures microcrack; then, the initial damage compliance matrix due are adopted to be -20°C and 20°C, respectively. The time of to one single microcrack is given by [25] one freeze-thaw cycle is 12 h. The detailed calculation method of Rf has been introduced by Walder and Hallet [28]. T ½C = ½C0 + ½Ai −1 ½ΔCi ½Ai −1 , ð19Þ Therefore, the variation of the frost heaving pressure with time is shown in Figure 2. where [C0 ] is the elastic compliance matrix, [Ai ] is the trans- The work done by the frost heaving pressure along the microcrack inner wall for one freeze-thaw cycle is formation matrix, and ½Ai −1 is its inverse matrix. ð ti ð ti 2 3 Δb Δb cos2 αi sin2 αi −sin 2αi W = 4api ðt Þ dt = 4a pi ðt Þdt, ð16Þ 6 7 6 sin 2αi 7 ½Ai = 6 sin αi cos2 αi ti ti 2 0 0 7, 4 5 1 1 where t i = 43200s and pi ðtÞ can be solved with Equation (14). sin 2αi − sin 2αi cos 2αi 2 2 2 3 3. Establishment of the Rock Constitutive cos αi 2 sin2 αi sin 2αi Model under Compression after Freeze- 6 7 6 −sin 2αi 7 ½Ai −1 = 6 sin αi cos2 αi 2 Thaw Cycles 7, 4 5 ð20Þ 1 1 sin 2αi − sin 2αi cos 2αi 3.1. Establishment of the Rock Constitutive Model. It is 2 2 assumed that the water/ice phase change in freeze-thaw con- 2 3 0 0 0 dition is the main reason leading to rock deterioration. The 6 7 frost heaving pressure is generated by 9% volume expansion 6 C in aim 7 60 0 7 of freezing water in closed microcrack. The pressure makes 6 ½ΔCi = 6 i K n 2dh 7 7 the microcrack propagate and when the temperature rises, 6 7 4 C is aim 5 the melt water will go into the newly formed microcracks. 0 0 The repeated freeze-thaw cycles cause continuous damage K is 2dh to the rock. Based on this viewpoint, the propagation of one single microcrack under the frost heaving pressure is studied, where C in , C is , K in , and K is are the compression transferring and the relationship between the propagation length of the coefficient, shear transferring coefficient, normal stiffness, microcrack and the frost heaving pressure is obtained. and shear stiffness of the ith crack, respectively. d and h are Because new damage continuously occurs under freeze- width and height of the rock sample, respectively. thaw cycles, the elastoplastic theory is adopted to study the The total compliance matrix including N microcracks rock damage mechanical behavior, and finally, a new consti- whose half-length am is tutive model for a rock based on the deformation and prop- agation of microcracks under compression after freeze-thaw N T cycles is proposed. ½C = ½C0 + 〠 ½Ai −1 ½ΔCi ½Ai −1 : ð21Þ i=1 3.2. Strain Decomposition. In this proposed model, the total strain of the rock under compression can be decomposed The orientation and size of the microcracks in the rock into the following four components such as the initial dam- are assumed to be random, which can be expressed with a
Geofluids 5 probability density function ρða, αÞ = ρðaÞρðαÞ. According ¦1Ò to the distribution law of the microcrack, its orientation and size satisfy the following normalization condition [30]: ð amax ð π/2 ρðaÞda ρðαÞ sin αdα = 1: ð22Þ l amin 0 ¦3Ò 2h ¦Á 2a Assume the total number of the microcracks is N c , and then, the number N of the microcracks with half-length of a can be expressed as ða 2d N = Nc ρðaÞda: ð23Þ amin Figure 3: The sliding microcrack model under compression. 2a and Assume the orientation of the microcrack evenly distrib- α are the length and dip angle of the microcrack, respectively. l is the utes in all directions [31], and according to the definition of wing crack length. 2h and 2d are the height and width of the model, the density function, ρðαÞ = 1 is obtained. Therefore, the total respectively. compliance matrix including all microcracks is ð amax ð π/2 −1 T −1 factor K I at the microcrack tip is [31, 33] ½C = ½C 0 + N c ½Ai ½ΔC i ½Ai ρðaÞda sin αdα: amin 0 ð24Þ 2 pffiffiffiffiffiffiffiffiffi K I = pffiffiffi τ∗ πam , ð27Þ With Equation (24), the initial damage compliance 3 matrix for different freeze-thaw cycles can be calculated and then, the initial damage strain can be finally obtained. where τ∗ is the effective shear stress on the microcrack face, τ∗ = τm − f σm , τm and σm are the shear and normal stresses 3.2.2. Elastic Strain. For a plane stress issue, the elastic consti- on the microcrack face, respectively, and f is the friction tutive relationship of rock is [32] coefficient of the microcrack face. ½εe = ½C0 ½σ, ð25Þ σ1 − σ3 where ½εe is the elastic strain matrix, ½εe = ½ε11 ε33 ε13 T , ½σ is τm = sin 2α, the stress matrix, ½σ = ½ σ11 σ33 σ13 , and ½C0 is the elas- 2 ð28Þ σ + σ3 σ1 − σ3 tic compliance matrix, σm = 1 − cos 2α: 2 2 2 3 1 ν 6 E − 07 When K Ι ≥ K IC (K IC is the rock fracture toughness), the 6 E 7 6 ν 7 microcrack begins to propagate, and the stress intensity fac- 6 1 07 ½C0 = 6 − 7, ð26Þ tor K W I at the wing crack tip is [31, 33]. 6 E E 7 6 7 4 15 0 0 μ 2aτ∗ cos α pffiffiffiffiffi KW I = pffiffiffiffiffi − σ3 πl, ð29Þ πl where E, μ, and υ are the rock elastic modulus, shear modu- lus, and Poisson ratio, respectively. where 3.2.3. Additional Damage Strain due to Compression. Under compression, the microcrack will firstly close, and then, the friction occurs along the microcrack face. When the shear 1 stress along the microcrack face is larger than the friction, τ∗ = ½ðσ − σ3 Þ sin 2α − f ðσ1 + σ3 + ðσ1 − σ3 Þ cos 2αÞ: 2 1 the wing crack will initiate and propagate from the micro- crack tip. The propagation of the microcrack will lead to ð30Þ the decrease in the rock elastic modulus, strength, and increase in the rock permeability. The sliding microcrack Ι ≤ K IC , so The wing crack will stop propagating when K W model under compression is shown in Figure 3. l can be calculated with Equation (29). After m freeze-thaw cycles, the microcrack length The additional damage of a rock is due to the wing becomes am , and for this moment, the first stress intensity crack propagation. According to Li and Lajtai [34], the
6 Geofluids macroscopic strain of a rock can be calculated. 10000 ac = 0.0001m ∗ 8λχ cos α 2τ cos α l l 8000 ε∗1 = ln − σ3 −1 , π (a)/ 1 (m) E a a 2 !3 6000 16τ∗ γ cos2 α l l2 6 ln + σ3 π 2 − 1 7 ð31Þ 4000 χ6 π a a 7 ε∗3 = 66 7, 7 E4 l 5 2000 ∗ −8 cos α − 1 ðσ3 γ + τ Þ a 0 1E–7 1E–6 1E–5 1E–4 where ε∗1and ε∗3 are the strains along the vertical and hor- a (m) izontal directions, respectively; λ = sin α cos α − f cos2 α; γ = −cos α sin α − f sin2 α. χ is defined as the initial micro- Figure 4: Probability density functions of the microcracks. crack density and is expressed as χ = Na2 /V. N is the total number of the microcracks in a two-dimensional body of unit thickness whose volume is V = 2 h × 2d. with the freeze-thaw cycles and obeys the following exponen- Finally, the total rock strain due to compression consid- tial function: ering the normalization condition is ð amax ð π/2 cðmÞ = c0 e−0:072m , ð35Þ 8λχ cos α ε1 = N c ρðaÞda ρðαÞ sin αdα ⋅ amin 0 E where c0 is the original cohesion strength (before freeze-thaw 2τ∗ cos α l l cycle) and cðmÞ is the cohesion after the mth freeze-thaw × ln − σ3 −1 , π a a cycle. The plastic strain rate is ð amax ð π/2 χ ε3 = N c ρðaÞda ρðαÞ sin αdα ⋅ E ∂G " amin 0 ! ε_ p = λ_ , ð36Þ ∂σ 16τ∗ γ cos2 α l l 2 × ln + σ3 π 2 − 1 ð32Þ π a a where λ_ is a proportion coefficient. l − 8 cos α − 1 ðσ3 γ + τ∗ Þ : 3.2.5. The Number of the Microcracks in a Rock. The proba- a bility function [37] of the microcrack length can be expressed as 3.2.4. The Plastic Strain due to Compression. The Drucker- Prager model is adopted to describe the rock plastic 8 behavior, whose yield function and plastic potential func- > < − 1 exp − a , a ≤ a ≤ a , min max tion are ρðaÞ = ac ac ð37Þ > : pffiffiffiffi 0, otherwise, F ðσ, κÞ = β1 I 1 +J 2 − κ, pffiffiffiffi ð33Þ Gðσ, κÞ = β2 I 1 + J 2 − κ, where ac is the characteristic length of the microcrack, ac = Ð amax amin ρðaÞada. N c is the total number of the microcracks per where I 1 = σ1 + σ2 + σ3 , J 2 = ð1/6Þ½ðσ1 − σ2 Þ2 + ðσ2 − σ3 Þ2 unit volume, which is determined by the total volume of pffiffiffi pffiffiffi Ð + ðσ3 − σ1 Þ2 , β1 = 2 sin φ/ 3ð3 − sin φÞ, β2 = 2 sin ψ/ 3ð the microcrack, V c = 2πbN c aamax ρðaÞa2 da. 3 − sin ψÞ, and φ and ψ are the friction angle and dilation min Finally, the curve of probability density function of the angle, respectively. κ is the hardening function, which can microcracks is shown in Figure 4. be expressed as [35] According to the experiment result of Rostásy et al. [38], the total number of the microcracks basically remains the κ = σ0 + a1 λ exp ða2 I 1 − a3 λÞ, ð34Þ same after freeze-thaw cycles. The longer microcracks will propagate, while the shorter ones will close under the extru- where a1 , a2 , and a3 are the constants which can be sion of other microcracks. Therefore, it is assumed that the obtained by fitting with thepffiffiuniaxial ffi compressive stress- total volume of the microcrack is the same during the strain curve. σ0 = 6c cos φ/ 3ð3 − sin φÞ; c is the rock freeze-thaw cycles and compression. So the total volume V c cohesion. of the microcracks can be expressed with the rock void According to Tan et al. [36], the rock internal friction porosity e and the total volume V of the rock sample, namely, angle is basically the same, but the rock cohesion decreases V c = eV.
Geofluids 7 0.010 100000 ac = 0.0001m 0.008 80000 Numbers of cracks N 0.006 acr (m) 60000 0.004 0.002 40000 0.000 20000 0 10 20 30 40 50 60 0 (MPa) 0 20 40 60 80 100 120 140 Figure 5: Relationship between the microcrack critical length and (MPa) axial stress. Figure 6: Relationship between the microcrack initiation number and axial stress. The first stress intensity factor K I of the microcrack with different lengths at the same stress condition can be tri ¦n+1 Ò expressed as rn ¦n+1Ò fn+1 2 pffiffiffiffiffiffi K I = pffiffiffi τ∗ πa: ð38Þ ¦nÒ fn 3 Equation (38) can be changed into pffiffiffi !2 3K IC 1 Figure 7: Graphic returns method of semi-implicit integration = acr , ð39Þ algorithm. 2τ∗ π (2) Update stresses and plastic strain and hardening where τ∗ = ð1/2Þ½ðσ1 − σ3 Þ sin 2φ − f ðσ1 + σ3 + ðσ1 − σ3 Þ function κn+1 cos 2φÞ where acr is the critical length of the microcrack which becomes active at the condition of σ1 and σ3 when K Ι = K IC . p As shown in Figure 5, the microcrack whose length is εn+1 = εpn + Δλn+1 rn , greater than acr will propagate. κn+1 = κn Δλn+1 hn The total number of microcracks Ð that will be actually ð41Þ p activated is given by N = N c aamax ρðaÞda, as shown in σn+1 = C−1 : εn+1 − εn+1 min Figure 6. F n+1 = F ðσn+1 , κn+1 Þ = 0 3.2.6. The Numerical Algorithm of the Proposed Model. The calculation of the rock plastic strain at different times where r n = ∂G/∂σjσ=σn and hn = ∂κ/∂κjλ=λn . can be calculated with the semi-implicit return graphical algorithm [17], shown in Figure 7. The plastic variables Calculate the plastic internal variable Δλn+1 : p σn+1 , εn+1 , κn+1 , rn+1 , and hn+1 at t n+1 are determined by integration flow rule and hardening law and Δσtr , σn , κn , akn+1 + C −1 : Δσkn+1 + δλk rn = 0, ð42Þ r n = ∂F/∂σjσ=σn , and hn = ∂κ/∂λjλ=λn at time t n . The main steps are as follows: (1) Update strain tensor, and calculate the elastic strain bkn+1 −Δκkn+1 + δλkn+1 hn = 0, ð43Þ at time t n+1 εn+1 = εn + Δε, ð44Þ ð40Þ F kn+1 + F kσ : Δσkn+1 + F kκ ∙Δκkn+1 = 0, −1 Δσtrn+1 =C : Δε, " # where C is the initial elastic compliance matrix Δσ h ih i h i including the initial damage compliance tensor = − AðkÞ ~aðkÞ − δλðkÞ AðkÞ ½~r n , ð45Þ caused by freeze-thaw and elastic compliance tensor. Δκ
8 Geofluids 200 240 160 200 1– 3 (MPa) 160 1– 3 (MPa) 120 120 80 80 40 40 0 0.000 0.002 0.004 0.006 0.008 0 0.000 0.002 0.004 0.006 0.008 Axial strain Axial strain m = 0 test result #1 m = 0 test result #2 m = 0 test result #1 m = 0 test result #3 m = 0 test result #2 m = 0 simulated with the m = 0 simulated with the proposed model proposed model 160 200 160 120 1– 3 (MPa) 1– 3 (MPa) 120 80 80 40 40 0 0 0.000 0.002 0.004 0.006 0.008 0 0.002 0.004 0.006 0.008 0.01 Axial strain Axial strain m = 50 test result #1 m = 50 test result #1 m = 50 test result #3 m = 50 test result #2 m = 50 simulated with the m = 50 simulated with the proposed model proposed model 120 160 120 1– 3 (MPa) 80 1– 3 (MPa) 80 40 40 0 0 0.000 0.002 0.004 0.006 0.008 0.000 0.002 0.004 0.006 0.008 Axial strain Axial strain m = 100 test result #1 m = 100 test result #1 m = 100 test result #2 m = 100 test result #2 m = 100 test result #3 m = 100 test result #3 m = 100 simulated with the m = 100 simulated with the proposed model proposed model Figure 8: Comparison of the stress-strain relationships for triaxial Figure 9: Comparison of the stress-strain relationships for triaxial compression tests with confining pressure σ3 = 5 MPa by Tan et al. compression tests with confining pressure σ3 = 10 MPa by Tan [36] and simulated with the proposed model. The predicted stress- et al. [36] and simulated with the proposed model. The predicted strain relationships agree well with the tested ones. stress-strain relationships agree well with the tested ones.
Geofluids 9 Table 1: The calculation parameters. E (GPa) v e c (MPa) a1 (MPa) a2 (MPa-1) a3 ac (m) amin (m) amax (m) 36.71 0.2 0.0067 27.43 5e9 1e-8 100 1e-4 1e-7 0.0012 where Update the length of wing crack ln+1 " # h i C 0 A k = , 2aðτÞn+1 cos φ pffiffiffiffiffiffiffiffiffiffi −I 0 KW I = pffiffiffiffiffiffiffiffiffiffi − ðσ3 Þn+1 πln+1 , ð52Þ πln+1 " k# " # h i a 0 ~að Þ = k = , ð46Þ where K W I = K IC . bk 0 Update the additional strain " # rn ½~rn = :: ð amax ð π/2 hn 8λa cos2 α ðε1 Þn+1 = N n+1 ρðaÞda ρðαÞ sin αdα ⋅ ðacr Þn+1 0 E δλðkÞ can be obtained with Equation (45) ∗ 2ðτ Þn+1 cos α ln+1 l × ln − σ3 n+1 − 1 , π a a Fk δλ = , ð47Þ ð amax ð π/2 ∂F : Ak : ~rn a2 ðε3 Þn+1 = N n+1 ρðaÞda ρðαÞ sin αdα ⋅ ða Þ 0 E 2 cr n+1 !3 where ½∂F = ½ F σ F κ . 16ðτ∗ Þn+1 γ cos2 α ln+1 ðln+1 Þ2 6 ln + σ3 π −1 7 6 π a a2 7 Δλk+1 6 7: n+1 = Δλn + δλ : ð48Þ k k ×6 7 6 7 4 ln+1 ∗ 5 −8 cos φ − 1 σ3 γ + ðτ Þn+1 a ð53Þ (3) Update N n+1 which is the number of microcracks that begin propagating At time t n+1 , the updated normal stress is σn+1 , under which the critical initiation length ðacr Þn+1 of the microcrack (5) Update the stress is calculated by pffiffiffi !2 σ∗n+1 = σn+1 − C−1 : ðεad Þn+1 ð54Þ 1 3K IC ðacr Þn+1 = , ð49Þ π 2ðτ∗ Þn+1 4. Verification of the Proposed Model where In order to verify the proposed model, the experiment by " # Tan et al. [36] is taken for an example. The rock type is 1 ðσ1 Þtrn+1 − σ3 sin 2φ granite, which is obtained from Galongla mountain in ðτ∗ Þn+1 = 2 −μðσ Þtr + σ +ðσ Þtr − σ cos 2φ , Tibet of China, where a highway tunnel passes through 1 n+1 3 1 n+1 3 the mountain and it is very cold in winter. The tested ð amax samples are prepared as cylinders with 50 mm in diameter N n+1 = N c ρðaÞda: and 100 mm high. The compression tests with confining ðacr Þn+1 pressure 5 MPa and 10 MPa on the rock sample are done ð50Þ with a multifunction rock mechanics test machine, and the corresponding stress-strain curves are shown in Figures 8 and 9. The calculation parameters are shown in Table 1. (4) Update the additional damage strain ðεad Þn+1 The characteristic length ac of the microcrack under 0, 50, and 100 freeze-thaw cycles is solved to be 0.1 mm, The additional damage strain matrix of εad can be 0.41 mm and 1.64 mm, respectively, with Equation (13). expressed as According to the proposed model, the complete stress- strain curve of the rock under compression with confining ½εad = ½ ε1 ε3 0 : ð51Þ pressure σ3 = 5 MPa/10 MPa is shown in Figures 8 and 9.
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