1 Introduction

Hydraulic fracturing is a critical technology for the high-efficiency development of unconventional hydrocarbon reservoirs, such as tight sandstones and shale gas. Many unconventional hydrocarbon reservoirs occur in formations with clear interfaces, such as stratified formations and formations interlaced with sand–mud beddings. A formation interface complicates the mechanism of hydraulic fracture propagation, owing to the difference in pressure, rock material properties, interfacial strength, interfacial morphology, and rock failure behavior between the two sides of the formation interface (Guo et al. 2017; Li et al. 2018; Lu et al. 2015; Tang et al. 2019). When hydraulic fractures extend to the vicinity of the formation interface but do not contact the formation interface, it can be considered that the hydraulic fractures are propagated in a homogeneous medium. Whereas the fracture is not in contact with the formation interface, the stress field of the fracture propagation interacts with it. When the resulting stress is large enough at the formation interface, the formation interface deforms and fails. The deformation and failure of the formation interface significantly influence fracture propagation, particularly in the height direction (Arash and Olson 2013; Bunger et al. 2012; Cohen et al. 2017; Jeffrey and Bunger 2009; Wang 2015, Wang et al. 2015). Therefore, it is necessary to analyze the stability of the formation interface under the impact of hydraulic fracture propagation in the vicinity of the formation interface.

Renshaw and Pollard (1995) suggested discontinuous fracture propagation across formation interfaces under the condition of small-range yields. More specifically, when a fracture impinges upon a formation interface oriented normal to the growing fracture, a new fracture can initiate at the other side of the formation interface. However, the old and new fractures do not form a continuous fracture. Wu et al. (2004) developed a fracture mechanism map, in which the behavior of a fracture propagating in the vicinity of a formation interface was considered. They found that a fracture propagating in the vicinity of an interface could induce a new fracture at the other side of the formation interface or bend. It may propagate in different morphologies simultaneously. They also found that, when in contact with the formation interface, the growing fracture could terminate at or cross the formation interface or propagate along it. Their subsequent experimental observations verified the above mechanisms. Their research results expanded the understanding of the mechanism of fracture propagation interacting with the formation interface. Stratum stress is a major factor influencing fracture propagation. When propagating from a lower-stress stratum to a higher-stress stratum, a fracture changes its direction in most cases. It usually breaks through the formation interface and terminates after propagating for a small distance (Warpinski and Teufel 1987; Zhao et al. 2009). When a fracture propagates near but does not contact an interface, the stress field at the fracture tip is the same as that in the case of a fracture propagating in a single-phase material (Irwin 1957). When a fracture propagates in a two-phase material, and the material surrounding the fracture tip is a single-phase material, the stress field at the fracture tip always has the singularity of r−1/2 (Kuang and Ma 2002). Lithological properties affect the behavior of a fracture propagating in the vicinity of a formation interface. However, they are not enough to explain fracture propagation in the vicinity (Daneshy 1978). Lithological properties affect the distribution of the stress field and the width of the fracture (Ham 1982). For a fracture propagating from a stratum with a lower Young’s modulus to a stratum with a higher Young’s modulus, the stress intensity factor decreases when the fracture approaches the formation interface and rapidly increases after it breaks through the formation interface (Hanson and Shaffer 1980). The difference in material properties between the two sides of the formation interface complicates the fracture propagation mechanism (Wu et al. 2004).

Many theoretical studies have been published on hydraulic fracture growth and containment in layer media (Chen et al. 2017; Damani et al. 2018; Garavand and Podgornov 2018; Ouchi et al. 2017a, b; Oyedokun and Schubert 2017; Paul et al. 2018; Tang and Wu 2018; Wang 2015, Wang et al. 2015; Zeng et al. 2018; Zhang et al. 2018). Fisher and Warpinski (2012) indicated that weak interfaces are regarded as a significant factor in stopping fracture height growth at shallow depths, initiating interface fractures or creating offsets along the interface. Rutledge et al. (2014) presented a model with step-over features to describe the sliding along the bedding interface which was driven by the opening of the vertical fracture. Chuprakov and Prioul (2015) elaborated a FracT model which can solve the problem of elasto-frictional fracture contact with weak horizontal interfaces. Cohen et al. (2017) proposed a new stacked height growth model (SHG), regarded as an enhanced pseudo-3D model (P3D), to model the effect of ledges at weak interfaces. Izadi et al. (2017) developed a fully coupled 3D hydraulic fracturing simulator to investigate interference of multiple fractures with consideration of the effect of bedding planes. Tang and Wu (2018) introduced a fully three-dimensional displacement discontinuity method (3D DDM) to model multiple fractures in three dimensions under the influence of weak interfaces.

Anderson (1981) observed the existence of critical normal stress through the interface in multi-layer fracture propagation simulation experiment. He proposed to use critical normal stress to judge whether the fracture passes through the interface. Biot et al. (1983) assumed that the fracture is shaped like a sine function and deduced the expression of the pressure inside the fracture when the fracture does or does not pass through the interface with the principle of virtual work, and by comparison of which, they proposed to judge whether the fracture has passed through the interface by the product of the surface energy and elasticity modulus of the fracture. Warpinski and Teufel (1987) proposed that the fracture propagates along the interface when the shear stress on the tip of the fracture paralleling to the interface is larger than the shear strength of the interface. He and Hutchinson (1989) proposed a method for judging whether a fracture passes through an interface by the energy release rate of the fracture tip. Renshaw and Pollard (1995) proposed two conditions for the crack to pass through the interface, one is that the tensile stress at the interface of the crack tip is greater than the tensile strength of the interface, and the other is that the shear stress at the crack tip along the interface is less than the shear strength of the interface. A stress analysis reported by Wu et al. (2004) suggests plane/straight fracture propagation when a fracture grows from a stiff to a soft material. Depending on the specifics of a given problem, an amount of fracture behavior can arise when a fracture propagates from a soft to a stiff material. Such behavior includes crack arrest at the interface, plane fracture growth, fracture kinking, interface delamination, and formation of secondary fractures. Some experimental evidences of these fracture behavior are reported in Wu et al. (2004) as well.

Researchers have done a lot of very valuable work on the fracture propagation model for layered formations. However, there is little concern about the stress field at the interface considering the heterogeneity of the formation, tip plastic zone and the dip angle of the formation, especially when the fracture does not touch the formation interface. In addition, the expansion criteria for fracture propagation to the interface are more complex than homogeneous formations due to the diversity of the expansion criteria. For this study, a model, considering the differences in rock mechanical properties on both sides of the formation interface and the influence of formation dip, was developed for computing the stress field of hydraulic fracture propagation near the formation interface. The effect of the plastic zone at the hydraulic fracture tip on the formation interface is discussed, and the stress fields within the formation, at the formation interface, and at the two sides of the formation interface are analyzed. The study identifies four failure modes of the formation interface under the impact of hydraulic fracture propagation in the vicinity of the formation interface and proposes corresponding failure criteria. Finally, the effect of different parameters (e.g., rock mechanical parameters, dip angle, distance between the hydraulic fracture and the formation interface, pump rate) on the failure mechanism and stability of the formation interface is analyzed.

2 Analysis of the stress field of fracture propagation near the formation interface

Lu et al. (2016) established a stress-field calculation model for propagating hydraulic fractures at the formation interfaces based on the complex variable function method and fracture mechanics theory. The propagation of hydraulic fractures at the formation interface was simplified to facilitate the computation, as shown in  Fig. 1 (Lu et al. 2016).

Fig. 1
figure 1

Modified from Lu et al. (2016)

Simplified diagram of the geometric model.

Based on the superposition principle, the propagation of the hydraulic fracture at the formation interface can be defined as the superposition of three issues: the fluid pressure pf in the hydraulic fracture without far-field stress; that with far-field stress and without hydraulic fracture; and the self-balancing surface force on the surface of the hydraulic fracture without far-field stress.

Using the superposition principle, a model is obtained to calculate the extended stress field of hydraulic fracture at the interface of the formation, and the corresponding Cauchy singular integral equations are established. The numerical solution is proposed based on the Lobatto–Chebyshev quadrature method. The simplified model and the stress field calculation model of the type I Griffith crack subjected to the uniaxial tension problem show that the model is correct and reliable.

2.1 Plastic zone at the hydraulic fracture tip

To avoid the effect of stress singularity, we assume that there exists plastic yield in a small zone at the fracture tip (Fig. 2). A hydraulic fracture propagating in the vicinity of a formation interface can be taken as one in a homogeneous medium. Thus, only the plastic zone at the fracture tip in the lower stratum is analyzed. The von Mises yield criterion was used to determine the size of the plastic zone at the hydraulic fracture tip:

$$\left[ {\sigma_{{{\text{s}}xx}} \left( {r_{1} } \right) - \sigma_{{{\text{s}}yy}} \left( {r_{1} } \right)} \right]^{2} + 6\left[ {\sigma_{{{\text{s}}xy}} \left( {r_{1} } \right)} \right]^{2} = 2\sigma_{{{\text{s}}1}}^{2} = 6\tau_{{{\text{s}}1}}^{2}$$
(1)
Fig. 2
figure 2

Plastic zone at fracture tip (Fan 1978)

Assuming that the rock in the plastic zone is in an idealized plastic status, the stress in the rock is smaller than or equal to the stress at the boundary of the plastic zone (Gu et al. 2012). The stress field at the formation interface is computed using the models for computing the stress field of hydraulic fracture propagation in the vicinity. The radius of the plastic zone at the fracture tip is then determined using Eq. (1). The distance between the hydraulic fracture and the formation interface is set to 0.5 m, and the other parameters are set to values given by Lu et al. (2016), as shown in Table 1.

Table 1 Basic parameters for the computation

As shown in Fig. 3, the plastic zone at the hydraulic fracture tip is small, when the growing hydraulic fracture is not in contact with the formation interface. Its boundary is not in contact with the formation interface, and it has a small effect on the stress field at the formation interface. Therefore, the effect of the plastic zone at the fracture tip is not considered in the examination of hydraulic fracture propagation in the vicinity of formation interface. Instead, the stress field at the formation interface is directly analyzed and computed.

Fig. 3
figure 3

Plastic zone at the tip of a hydraulic fracture propagating in the vicinity of a formation interface

2.2 Analysis of the stress field

The stress field of hydraulic fracture propagation in the vicinity of formation interface is computed using the models proposed above. The maximum principal stress, normal stress, and shear stress at the formation interface are then analyzed separately for their distribution characteristics.

2.2.1 Within-formation stress fields

Table 1 shows the parametric setting for the computation. A computational program was written in the MATLAB software to compute the maximum normal stress field and shear stress field in the formation and the stress field normal to the formation interface. The computation step length was 0.1 m. Figures 4, 5 and 6 show the computational results.

Fig. 4
figure 4

Maximum normal stress fields in the formation

Fig. 5
figure 5

Normal stress fields in the strata

Fig. 6
figure 6

Shear stress fields in the strata

The within-formation stress fields of hydraulic fracture propagation in the vicinity of the formation interface have the following characteristics:

  • A stress field with stress concentration was induced around the hydraulic fracture. As the effect of the plastic zone at the fracture tip was neglected, the fracture tip exhibited stress singularity.

  • The maximum normal stress field and normal stress field are symmetric, whereas the shear stress field is antisymmetric.

  • As the distance to the hydraulic fracture increases, the maximum normal stress field and normal stress field gradually transit from tensile to compressive. The direction of the shear stress in the formation changes with the angle relative to the hydraulic fracture.

2.2.2 Stress field at the formation interface

Assuming the hydraulic fracture propagation remains within the lower stratum, the stress field of the upper and lower strata of the interface under different rock mechanical properties is calculated. The variation trends of the stresses at the two sides of the formation interface are then computed. When there is a difference between the upper and lower sides, we define that the pay layer has a high Young’s modulus and a low Poisson’s ratio, correspondingly, the barrier is just the opposite. When there is no difference between the upper and lower sides, the rock mechanical properties are the same. Table 2 shows the setting for rock mechanical parameters used in the computation. The setting for other parameters is shown in Table 1. Figures 7, 8 and 9 show the computational results.

Table 2 Setting for rock mechanical parameters for different configurations
Fig. 7
figure 7

Maximum normal stress fields at the two sides of the formation interface under different rock mechanical parameters. a Hydraulic fracture within the pay layer. b Hydraulic fracture within the barrier bed. c No difference between pay layer and barrier bed

Fig. 8
figure 8

Normal stress fields at the two sides of the formation interface under different rock mechanical parameters. a Hydraulic fracture within the pay layer. b Hydraulic fracture within the barrier bed. c No difference between pay layer and barrier bed

Fig. 9
figure 9

Shear stress fields at the two sides of the formation interface under different rock mechanical parameters. a Hydraulic fracture within pay layer. b Hydraulic fracture within barrier bed. c No difference between pay layer and barrier bed

The stress fields at the two sides of the formation interface resulting from hydraulic fracture propagation in the vicinity of the formation interface have the following distribution characteristics:

  • When the upper side and the lower side are of different properties, the maximum normal stresses, normal stresses, and shear stresses at the two sides of the formation interface vary at different slopes. The stress-change rate in the side with high Young’s modulus and low Poisson’s ratio is bigger than that in the side with low Young’s modulus and high Poisson’s ratio.

  • The maximum normal stresses at the two sides of the formation interface are discontinuous. The maximum tensile stress at the pay-layer side of the formation interface is bigger than that at the barrier-side of the formation interface. This indicates that the pay layer has a higher tendency of tensile failure than the barrier bed, and the barrier bed serves to contain fracture propagation in the height direction. The discontinuous distribution of the maximum normal stresses is caused by the difference in stress between the pay layer and the barrier bed and the discontinuous stresses induced at the two sides of the formation interface. Therefore, the lower and upper strata of the formation interface should be examined separately for the occurrence of tensile failure.

  • As the distance to the hydraulic fracture increases, the within-formation maximum normal stress field and normal stress field gradually transit from tensile to compressive. This indicates the reversal of the stresses at the two sides of the formation interface. As the distance to the hydraulic fracture increases, the stresses at the two sides of the formation interface gradually recover to the corresponding far-field stresses.

2.2.3 Stress fields at the two sides of the formation interface

When the rocks at the two sides of the formation interface are of different properties, the maximum normal stresses at the formation interface are discontinuous. Therefore, the stress fields at the upper and lower sides of the formation interface should be computed separately for analyzing the stress field. The normal compressive stress and shear stress are continuous at the formation interface. Thus, their distributions at only one side should be analyzed. Figures 10, 11, 12, 13, 14, 15 and 16 show the computational results.

Fig. 10
figure 10

Maximum normal stress at the formation interface at a dip angle of 0°

Fig. 11
figure 11

Direction of minimum normal stress at the formation interface at a dip angle of 0°

Fig. 12
figure 12

Normal compressive stress at the formation interface at a dip angle of 0°

Fig. 13
figure 13

Shear stress at the formation interface at a dip angle of 0°

Fig. 14
figure 14

Maximum normal stress at the formation interface at a dip angle of 45°

Fig. 15
figure 15

Normal compressive stress at the formation interface at a dip angle of 45°

Fig. 16
figure 16

Shear stress at the formation interface at a dip angle of 45°

At a dip angle of 0°, the stress fields at the formation interface have the following distribution characteristics:

  • The maximum tensile stress at the lower side of the formation interface is bigger than that at the upper side. At a point in the formation interface far away from the hydraulic fracture tip, the difference between the maximum normal stresses at the upper and lower sides of the formation interface is equal to the difference between the far-field stresses of the pay layer and barrier bed.

  • The maximum normal stress and normal stress distribute symmetrically around the hydraulic fracture. The tensile stress peaks at a point right above the hydraulic fracture. The shear stress exhibits an approximately antisymmetric distribution around the hydraulic fracture and peaks at a point slightly deviating from the normal direction of the hydraulic fracture

  • The minimum normal stress exhibits an antisymmetric distribution around the hydraulic fracture. More specifically, the minimum normal stress right above the hydraulic fracture is perpendicular to the formation interface. As the distance to the hydraulic fracture increases, the direction of the minimum normal stress rotates to the direction parallel to the formation interface.

  • As the distance between formation interface and hydraulic fracture increases, the normal stress gradually transits from tensile to compressive; the shear stresses at the two sides of the hydraulic fracture are in reverse directions and gradually recover to the corresponding far-field stresses.

As shown in Figs. 14, 15 and 16, at a dip angle of 45°, the maximum normal stress and normal compressive stress at the formation interface still exhibit symmetric, single-peak, and stress-reversal distributions. The shear stress at the formation interface still exhibits an antisymmetric, single-peak, and stress-reversal distribution. Note that, at a dip angle of 45°, the transition of the stress field at the formation interface is caused by the change in the position of the hydraulic fracture relative to the formation interface, and this does not affect the results of the stress-field analysis.

3 Criteria for determining the failure of the formation interface

Under the effect of the stress field caused by hydraulic fracture propagation near the formation interface, the formation interface may experience four different modes of failure: Type A failure (Fig. 17a), where tensile failure occurs at either or both sides of the formation interface with new fractures initiating at either or both sides of the formation interface; Type B failure (Fig. 17b), where shear failure occurs at the formation interface, resulting in a slip; Type C failure (Fig. 17c), where tensile failure occurs at the formation interface, with new fractures initiating at it; and complex failure (Type D failure) (Fig. 17d), where failure occurs at the formation interface and at either side of it, and the failure is a result of the occurrence of two or more of the above failure modes.

Fig. 17
figure 17

Potential failure modes of a formation interface under the impact of hydraulic fracture propagation near the formation interface

The above four failure modes are related to the magnitude of the stress acting on the formation interface and the criteria for determining the failure modes.

3.1 Criteria for tensile failure at either or both sides of the formation interface

Tensile failure of the rocks at either or both sides of the formation interface (i.e., Type A failure) can be determined using the maximum normal stress intensity theory. However, because the theory is only applicable to tensile status under two-dimensional stress conditions, its application to hydraulic fracture propagation near the formation interface requires the condition that the maximum principal stress acting on it be tensile and have a negative value.

3.1.1 Tensile failure of the lower stratum

The tensile failure of the lower stratum, designated as a Type A1 failure, can be determined with the following equation:

$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } > - T_{2} } \\ \end{array} } \right\}$$
(2)

The propagation direction of the new fracture developing in the lower stratum can be computed using the following equation:

$$\tan 2\theta_{1} = \frac{{2\sigma_{1xy} }}{{\sigma_{1xx} - \sigma_{1yy} }}$$
(3)

3.1.2 Tensile failure of the upper stratum

The tensile failure of the upper stratum, designated as a Type A2 failure, can be determined with the following equation:

$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } > - T_{1} } \\ \end{array} } \right\}$$
(4)

When the tensile failure occurs at either side of the formation interface, the propagation direction of the new fracture developing at it is the same as the direction of the minimum principal stress. The propagation direction of the new fracture developing in the upper stratum can be computed using the following equation:

$$\tan 2\theta_{2} = \frac{{2\sigma_{2xy} }}{{\sigma_{2xx} - \sigma_{2yy} }}$$
(5)

3.1.3 Tensile failure at both sides of the formation interface

The tensile failure at both sides of the formation interface, designated as a Type A12 failure, can be determined by the following equation:

$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ \end{array} } \right\}$$
(6)

The propagation direction of the new fractures developing at the two sides of the formation interface can be determined using Eqs. (3) and (5).

3.2 Shear failure of the formation interface

The shear failure at the formation interface, Type B failure, can be determined using the Mohr–Coulomb failure criterion (Xie and Chen 2004). According to the single-plane-of-weakness theory, the presence of a formation interface in rock mass results in the anisotropy of the rock mass in the height direction (Liu et al. 2013). Thus, when the shear failure occurs at the formation interface, the rock mass has the smallest shear strength, equalling the shear strength of the formation interface. Therefore, it is appropriate to use the Mohr–Coulomb failure criterion to determine whether the shear failure has occurred at the formation interface. A shear stress acts on the formation interface, satisfying the following equation:

$$\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}}$$
(7)

The shear failure of the formation interface is related to the shear stress and normal stress acting on the formation interface.

3.3 Tensile failure of the formation interface

The tensile failure at the formation interface is designated a Type C failure. Under normal stress, it experiences a normal deformation. When the normal stress is tensile, the formation interface experiences tensile failure. Like the maximum normal stress intensity theory, the failure criterion of the rock is:

$$\sigma_{yy} < - T_{\text{s}}$$
(8)

Note that this failure criterion is also based on the condition that the normal stress acting on the formation interface is tensile and has a negative value.

3.4 Complex failure

The complex failure is designated as a Type D failure. When the stress acting on the formation interface satisfies two or more failure criteria, the formation interface and the other side of the formation interface experience complex failure. The criteria for determining the complex failure can be expressed as Eqs. (9)–(18):

$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ {\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} > - T_{\text{s}} } \\ \end{array} } \right\} \quad {\text{Type A}}_{12} + {\text{Type B}}$$
(9)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ {\sigma_{xy} < \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} < - T_{\text{s}} } \\ \end{array} } \right\}\quad {\text{Type A}}_{12} + {\text{Type C}}$$
(10)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } > - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } > - T_{2} } \\ {\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} < - T_{\text{s}} } \\ \end{array} } \right\}\quad {\text{Type B}} + {\text{Type C}}$$
(11)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ {\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} < - T_{\text{s}} } \\ \end{array} } \right\}\quad {\text{Type A}}_{12} + {\text{Type B}} + {\text{Type C}}$$
(12)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } > - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ {\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} > - T_{\text{s}} } \\ \end{array} } \right\} {\text{Type A}}_{2} + {\text{Type B}}$$
(13)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } > - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ {\sigma_{xy} < \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} < - T_{\text{s}} } \\ \end{array} } \right\} {\text{Type A}}_{2} + {\text{Type C}}$$
(14)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } > - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } < - T_{2} } \\ {\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} < - T_{\text{s}} } \\ \end{array} } \right\} {\text{Type A}}_{2} + {\text{Type B}} + {\text{Type C}}$$
(15)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } > - T_{2} } \\ {\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} > - T_{\text{s}} } \\ \end{array} } \right\} {\text{Type A}}_{1} + {\text{Type B}}$$
(16)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } > - T_{2} } \\ {\sigma_{xy} < \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} < - T_{\text{s}} } \\ \end{array} } \right\} {\text{Type A}}_{1} + {\text{Type C}}$$
(17)
$$\left. {\begin{array}{*{20}l} {\frac{{\sigma_{1xx} + \sigma_{1yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{1xx} - \sigma_{1yy} }}{2}} \right)^{2} + \sigma_{1xy}^{2} } < - T_{1} } \\ {\frac{{\sigma_{2xx} + \sigma_{2yy} }}{2} - \sqrt {\left( {\frac{{\sigma_{2xx} - \sigma_{2yy} }}{2}} \right)^{2} + \sigma_{2xy}^{2} } > - T_{2} } \\ {\sigma_{xy} > \sigma_{yy} \tan \varphi_{\text{s}} + C_{\text{s}} } \\ {\sigma_{yy} < - T_{\text{s}} } \\ \end{array} } \right\} {\text{Type A}}_{1} + {\text{Type B}} + {\text{Type C}}$$
(18)

4 Analysis of the stability of the formation interface

The stability of the formation interface under the impact of nearby hydraulic fracture propagation with different conditions was analyzed based on the stress-field distribution at the interface and the corresponding criteria for the classification of fracture propagation. The stability of the formation interface refers to whether the interface is displaced and whether the upper and lower sides of the rock are failed. Therefore, by analyzing whether the formation interface is displaced and the rock is failed, the stability of the formation interface can be obtained. Considering that the rocks above and below the formation interface had different mechanical properties and stresses (Zhang and Jeffrey 2007), some variables were analyzed for their impact on its stability based on the setting for basic parameters given in Tables 1 and 3.

Table 3 Basic parameters for computation of hydraulic fracture propagation near the formation interface

4.1 Impact of rock mechanical properties on the shear and tensile failure modes of the formation interface

Table 4 shows Young’s modulus of the rocks at the two sides of the formation interface simulated for the analysis. The magnitude and direction of the peak stress at the formation interface at different Young’s modulus values of the rock below the formation interface were simulated and computed. On this basis and according to the criteria for fracture propagation classification, the stability of the formation interface under the impact of hydraulic fracture propagation near the formation interface was analyzed.

Table 4 Simulated Young’s modulus of the rocks at the two sides of the formation interface

The computational results (Fig. 18) show that, as Young’s modulus E of the rock below the formation interface increases, the formation interface is stable and then experiences the following modes of failure in sequence: Type B failure, Type A1 + Type B failure, Type A12 + Type B failure, Type A2 + Type B failure, Type A2 + Type B + Type C failure, and Type B + Type C failure. When E1 < 12,000 MPa, the formation interface is stable. When 12,000 ≤ E1 < 15,000, the shear stress acting on the formation interface exceeds the critical shear strength, and a slip occurs. When 15,000 ≤ E1 < 16,000, the maximum tensile strength acting on the upper side of the formation interface exceeds the critical shear strength of the rock above, a slip occurs, and tensile failure occurs in the rock above. When 16,000 ≤ E1 < 28,000, the maximum tensile stress acting on the lower side of the formation interface exceeds the critical tensile strength of the rock below, a slip occurs, and tensile failure occurs in the rock below. When 28,000 ≤ E1 < 30,000, the maximum tensile strength acting on the lower side of the formation interface is smaller than the critical tensile strength of the rock below the formation interface, a slip occurs, and the tensile failure occurs in the rock above. When 30,000 ≤ E1 < 50,000, the normal tensile stress acting on the formation interface exceeds its critical tensile strength, a slip occurs with tensile failure appears in the rock above. When E1 ≥ 50,000, the maximum tensile strength acting on the upper side of the formation interface is smaller than the critical tensile strength of the rock above, and a slip and tensile failure occur.

Fig. 18
figure 18

Shear and tensile failure modes of the formation interface under the impact of hydraulic fracture propagation near the formation interface at different Young’s moduli of the rock below the formation interface

The analysis reveals that, as Young’s modulus of the rock below the formation interface increases, the formation interface is more prone to slipping than tensile failure. Whether the rocks at its two sides experience tensile failure depends on the tensile strength of the rock matrix and the direction of the maximum tensile stress. As Young’s modulus of the rock below the formation interface increases, the complexity of the failure of the formation interface first increases, peaks when the rocks above and below have similar Young’s moduli, and then decreases. This indicates that, either the hydraulic fracture is propagating in the pay layer or the barrier bed, a big difference in Young’s modulus between the rocks above and below the formation interface serves to inhibit the initiation of new fractures at its two sides.

4.2 Shear and tensile failure modes of the formation interface at different dip angles

The magnitude and direction of the peak stress at the formation interface at different dip angles were simulated and analyzed. Its stability under the impact of nearby hydraulic fracture propagation was then analyzed.

The results (Fig. 19) show that, as the dip angle β increases, the formation interface is stable, experiences the following modes of failure, and recovers stability: Type B failure, Type A1 + Type B failure, Type A1 + Type B + Type C failure, Type A12 + Type B + Type C failure, Type A12 + Type B failure, Type A1 + Type B failure, and Type B failure. When β < 10°, the formation interface is stable. When 10° ≤ β < 28°, the shear stress acting on the formation interface exceeds its critical shear strength, and a slip occurs. When 28° ≤ β < 30°, the maximum tensile stress acting on the lower side of the formation interface exceeds the critical tensile strength of the rock below, a slip occurs, and tensile failure occurs in the rock below. When 30° ≤ β < 36°, the normal tensile stress acting on the formation interface exceeds its critical tensile strength, a slip and tensile failure occur, and tensile failure occurs in the rock below. When 36° ≤ β < 53°, the maximum tensile stress acting on the upper side of the formation interface exceeds the critical tensile strength of the rock above, a slip and tensile failure occur, and tensile failure occurs in the rock above. When 53° ≤ β < 55°, the normal tensile stress acting on the formation interface is smaller than its critical tensile strength, a slip occurs, and tensile failure occurs in the rocks below and above. When 55° ≤ β < 60°, the maximum tensile stress acting on the upper side of the formation interface is smaller than the critical tensile strength of the rock above, a slip occurs, and tensile failure occurs in the rock below. When 60° ≤ β < 80°, the maximum tensile stress acting on the lower side of the formation interface is smaller than the critical tensile strength of the rock below, a slip occurs. When β ≥ 80°, the shear stress acting on it is smaller than its critical shear strength, and it does not fail.

Fig. 19
figure 19

Shear and tensile failure modes of the formation interface under the impact of hydraulic fracture propagation near the formation interface at different dip angles

The analysis reveals that, as the dip angle approximates 45°, a slip at the formation interface has a higher possibility of occurrence than tensile failure at the two sides, followed by tensile failure at the formation interface. As the dip angle increases, the complexity of failure at the formation interface first increases then decreases, exhibiting a roughly symmetric pattern around a dip angle of 45°. There, the hydraulic fracture is most likely to cross the formation interface.

4.3 Shear and tensile failure modes of the formation interface at different distances to the hydraulic fracture

The magnitude and direction of the peak stress at the formation interface at different distances, C, between it and the hydraulic fracture was simulated and computed. The results (Fig. 20) show that, as C increases, the formation interface experiences the following different modes of failure in sequence and then recovers stability: Type A12 + Type B + Type C failure, Type A12 + Type B failure, and Type B failure. When C < 0.65 m, the normal tensile stress and shear stress acting on the formation interface and the maximum tensile stress acting on the rocks at its two sides are bigger than its corresponding critical strengths, a tensile and slip failure occurs, and tensile failure occurs in the rocks at the two sides. When 0.65 m ≤ C < 0.8 m, the normal tensile stress acting on the formation interface is smaller than its critical tensile strength, a slip occurs at the information interface, and tensile failure occurs in the rocks at the two sides. When 0.8 m ≤ C < 0.97 m, the maximum tensile stresses acting on the upper and lower sides of the formation interface are smaller than the critical tensile strengths of the rocks above and below the formation interface, and slip occurs at the formation interface. When C ≥ 0.8 m, the shear stress acting on the formation interface is smaller than its shear strength, and it does not fail.

Fig. 20
figure 20

Shear and tensile failure modes of the formation interface under the impact of hydraulic fracture propagation near the formation interface at different distances between the hydraulic fracture and the formation interface

The analysis reveals that, as the distance between the hydraulic fracture and the formation interface decreases, slip has a higher probability of occurrence than tensile failure in the rocks at the two sides, followed by tensile failure.

4.4 Shear and tensile failure modes of the formation interface at different pump rates

The magnitude and direction of the peak stress at the formation interface at different pump rates were simulated and computed. The results (Fig. 21) show that, as the pump rate, Q, increases, the formation interface is first stable and then experiences the following different modes of failure in sequence: Type B failure, Type A2 + Type B failure, Type A12 + Type B failures, and Type A12 + Type B + Type C failure.

Fig. 21
figure 21

Shear and tensile failure modes of the formation interface under the impact of hydraulic fracture propagation near the formation interface at different pump rates

When Q < 3 m3/min, the formation interface is stable. When 3 m3/min ≤ Q < 3.9 m3/min, the shear stress acting on the formation interface exceeds its critical shear strength, and a slip occurs. When 3.9 m3/min ≤ Q < 4.5 m3/min, the maximum tensile stress acting on the upper side of the formation interface exceeds the critical tensile strength of the rock above, a slip occurs, and tensile failure occurs in the rock above. When 4.5 m3/min ≤ Q < 6.4 m3/min, the maximum tensile stress acting on the lower side of the formation interface exceeds the critical tensile strength of the rock below, a slip occurs, and tensile failure occurs in the rocks above and below. When Q ≥ 6.4 m3/min, the normal tensile stress acting on the formation interface exceeds its critical tensile strength, a slip and tensile failure occurs, and tensile failure occurs in the rocks below and above.

The analysis reveals that, as the pump rate increases, a slip at the formation interface has a higher possibility of occurrence than tensile failure in the rock above, followed by tensile failure in the rock below and tensile failure at the interface. As the pump rate increases, the complexity of failure at the formation interface increases. For separate-layer fracturing at the formation interface, medium- to low-rate pumping is desirable for fracture height control, this means that with the simulation data of Fig. 21, the pump rate should be less than 3.9 m3/min. For simultaneous fracturing of multiple thin layers, medium- to high-rate pumping is desirable for improving reservoir utilization, taking the data in Fig. 21 as an example, the pump rate should be greater than 4.5 m3/min.

5 Conclusions

Criteria were proposed for determining the following four failure modes under the impact of hydraulic fracture propagation near the formation interface using the maximum normal stress intensity theory and the Mohr–Coulomb theory: tensile failure of rocks at either or both sides of the formation interface; shear failure at the formation interface; tensile failure at the formation interface; and complex failure.

The stress-field distribution in a layered formation under the impact of hydraulic fracture propagation near the formation interface is characterized by stress singularity and reversal. More specifically, the maximum normal stress field and normal stress field in the formation are symmetric. The shear stress field in the formation is antisymmetric. The maximum normal stress and normal stress field at the formation interface are symmetric with a single peak. The shear stress field is antisymmetric with a single peak, and the direction of minimum normal stress is antisymmetric.

When the pay layer and barrier bed are of different properties, the stress-change rate in the pay layer is bigger than that in the barrier bed. The maximum tensile stress at the pay-layer side of the formation interface is bigger than that at the barrier bedside. The major factors affecting the distribution and magnitude of the stress at the two sides of the formation interface include rock mechanical properties, distance between it formation interface and hydraulic fracture, and net pressure in the hydraulic fracture. The major factors affecting the stress-change rate at the two sides of the formation interface include rock mechanical properties and dip angle. The major factors affecting the discontinuity of the maximum normal stress at the two sides of the formation interface include rock mechanical properties.

At lower strengths of the formation interface, it fails before the growing hydraulic fracture is in contact. Its stability is significantly related to a variety of factors, including formation interface failure type, rock mechanical properties, far-field stress, structural parameters, distance between the formation interface and the hydraulic fracture, and fracturing execution parameters.