The PLT involves compressing of a brittle sample between two conical steel platens (pointers) until failure to evaluate its point load index (PLI or
\({I}_{\mathrm{s}}\)). In this study, for standard classification of such an index, the reference sample diameter of approximately 50 mm was used, and to obtain the optimum outcome, the rock samples were loaded under diametral and axial directions as suggested by ISRM (
1985). The diametral
\({I}_{\mathrm{s}}\) is defined according to
$${I}_{\mathrm{S}}=\frac{P}{{D}^{2}},$$
(1)
where
P is the maximum applied load and
D is the diameter of a sample which equals to the distance between the two pointers. Under axial point loading, the force is applied at the center of the end surfaces and the
\({I}_{\mathrm{s}}\) is estimated using the following equation:
$${I}_{\mathrm{S}}=\frac{P}{4LD/\pi },$$
(2)
where
L is the length of a sample and LD represents the minimum cross-sectional area of a plane through the pointers. Equations (
1) and (
2) were developed by Franklin (
1985) where the effect of contact surface area between the pointers and sample were not considered. Masoumi et al. (
2016) argued that the radius of the conical platens under point loading is important for estimation of PLI inspiring by the work conducted by Russell and Wood (
2009) who demonstrated that the contact area controls the stress intensity immediately below the contact points where the failure initiates. Thus, Masoumi et al. (
2016) included the contact area based on Timoshenko and Goodier’s (
1951) theory to introduce a more reliable estimation of point load index. The radius of contact area between two elastic spheres with different radii and mechanical properties can be calculated as follows:
$$r=\sqrt[3]{\frac{3\pi P({K}_{1}+{K}_{2}){R}_{1}{R}_{2}}{4 ({R}_{1}+{R}_{2})},}$$
(3)
where
R1 and
R2 are radii of two spheres; and
K1 and
K2 are calculated by the following equations:
$${K}_{1}=\frac{1-{v}_{1}^{2}}{\pi {E}_{1}}$$
(4)
$${K}_{2}=\frac{1-{v}_{2}^{2}}{\pi {E}_{2}},$$
(5)
where
\({v}_{1}\) and
\({v}_{2}\) represent Poisson’s ratios and
E1 and
E2 are Young’s moduli of two spheres. For simplicity, the surface roughness between the pointer and sample can be ignored as explained by Russell and Wood (
2009). The pointers are usually made of tungsten carbide or hardened steel, with a smooth and spherically curved tip of 5 mm as suggested by ISRM (Franklin
1985). The elastic modulus and Poisson’s ratio of tungsten carbide are about 700 GPa and 0.25, respectively (Russell and Wood
2009). Under diametral point loading, the contact area is elliptical shape as a pointer with a spherical tip pushes on a cylindrical surface. For typical elastic properties, the major and minor diameters in the ellipse have a ratio of one; therefore, the contact area can be assumed as a circle for simplicity.
As a result, the new PLI was proposed by Masoumi et al. (
2016) including the influence of contact area according to
$${I}_{\mathrm{s}(\mathrm{n})}=\frac{P}{A},$$
(7)
where
\({I}_{\mathrm{s}(\mathrm{n})}\) denotes the new PLI;
A is the contact area that can be estimated based on the radii obtained from Eqs. (
3) and (
6), for point loadings under diametral and axial directions, respectively. As explained earlier, a conventional regression to correlate UCS with PLI is
$$\mathrm{UCS}=k{I}_{\mathrm{s}},$$
(8)
where
k denotes index-to-strength conversion factor. The new correlations for relating UCS and PLI are derived through re-arranging Eq. (
8) and incorporating Eqs. (
1), (
2) and (
7) as follows:
$${\text{UCS}} = k\frac{A}{{D^{2} }}I_{{{\text{s}}({\text{nd}})}} \quad {\text{for}}\,{\text{diametral}}$$
(9)
$${\text{UCS}} = k\frac{A}{4LD/\pi }I_{{{\text{s}}({\text{na}})}} \quad {\text{for}}\,{\text{axial,}}$$
(10)
where
\({I}_{\mathrm{s}(\mathrm{nd})}\) and
\({I}_{\mathrm{s}(\mathrm{na})}\) represent new diametral and axial point load indices, respectively. As a result, the burst–brittleness ratio (BBR) is defined as follows;
$$\mathrm{BBR}=\frac{\mathrm{Compression\;conponent}}{\mathrm{Tensile\;component}}.$$
(11)
The compression component is estimated through UCS, while the
\({I}_{\mathrm{s}(\mathrm{na})}\) and
\({I}_{\mathrm{s}(\mathrm{nd})}\) derived from Eqs. (
9) and (
10) are substituted to tensile component leading to BBR for two different point loading directions as follows:
$${\text{BBR}}_{d} = \frac{{{\text{UCS}}}}{{I_{{s({\text{nd}})}} }} = k\frac{A}{{D^{2} }}\quad {\text{for}}\,{\text{diametral}}$$
(12)
$${\text{BBR}}_{a} = \frac{{{\text{UCS}}}}{{I_{{s({\text{na}})}} }} = k\frac{A}{4LD/\pi }\quad {\text{for}}\,{\text{axial,}}$$
(13)
where BBR
d and BBR
a represent the Burst–Brittleness Ratio for diametral and axial loading conditions, respectively. In principle, the BBR has the same characteristics as BI
1, but its tensile component is replaced by the new PLI proposed by Masoumi et al. (
2016). It is believed that incorporation of contact area in the proposed BBR can improve the accuracy of burst–brittleness assessment and can assist to make it more versatile for various rocks and different applications. Also, flexibility in performing point load testing is another major advantage of BBR over conventional BIs where PLI can be estimated very rapidly as opposed to other experiments, such as triaxial, direct/indirect tensile, and punch penetration tests. To assess the performance of the proposed BBR, three different rock types from various geological origins, including coal, granite, and sandstone, were selected for a comprehensive examination and their BBR, BI
1, and
k are compared. Also, the failure processes of tested rocks under uniaxial compression and point loading are visualized through high-speed imaging technique to then analyze their level of violent failure with the estimated BBR and BI
1.