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Rock strengths and rock failure criteria  89


              where P max is the maximum load exerted on the rock sample; A is the area
              of the cross section of the sample.
                 ISRM (1979) recommends that the test specimen should be a right
              circular cylinder, having a diameter approximately 54 mm, and a
              height-to-diameter ratio of 2.5e3. If thesamplesizedoesnot meet this
              requirement, the strength test results obtained from Eq. (3.2) will need to
              be corrected. Based on an analysis of a series of laboratory test data, Hoek
              and Brown (1980) found that rock UCS decreases as the sample size
              increases. They proposed that the UCS should be normalized by dividing
              individual strengthofeachsampletothe strength of asamplewitha
              diameter of 50 mm. The proposed correction is determined by the
              following equation:

                                                   0:18
                                               50
                                      s c ¼ s c50                         (3.3)
                                                d
              where s c is the corrected UCS for rock specimen with a diameter of
              d (mm); s c50 is the UCS for rock specimen with a diameter of d ¼ 50 mm.
                 Based on laboratory studies the rock failure process can be broken down
              into a number of stages characterized by changes in the measured axial and
              lateral strain response recorded during uniaxial and triaxial compression tests
              (Fig. 3.3). In the figure the axial and lateral strains are measured and the
              volumetric and crack volumetric strains are calculated. These stages include
              (Eberhardt et al., 1999):
              (1) Crack closure (at stress of s cc ).
                 Crack closure, at stress of s cc , occurs during the initial stages of loading
              when existing cracks orientated at an angle to the applied load close. During
              crack closure, the stressestrain response is nonlinear, exhibiting an increase
              in axial stiffness.
              (2) Linear elastic deformation (from s cc to s ci ).
                 Once the majority of existing cracks have closed, linear elastic defor-
              mation takes place.
              (3) Crack initiation and stable crack growth (from s ci to s cd ).
                 Crack initiation, s ci , represents the stress level where the loading-
              induced microfracturing begins. The growth of these cracks has been
              shown to occur in the direction of the major principal stress, s 1 , and cracks
              grow along a curved path to align themselves with s 1 . The opening of
              cracks with faces parallel to the applied load is therefore detected as a
              departure from linear lateral and volumetric strain behaviors.
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