Abstract
In this paper, white Portland cement was used as an experimental material. Prismatic specimens with pre-existing flaws at different angles of inclination (α) varying through 0°, 30°, 45°, 60°, 75° to 90° and cylindrical specimens with different numbers of pre-existing flaws (n) varying through 0, 1, 2 to 3 were tested under uni-axial compression tests. Crack initiation, propagation, coalescence, and failure were observed. The corresponding analytical expression for the stress intensity factor under uni-axial compression was derived, the coefficient of friction and the stress intensity factor of the specimens on the surfaces of the crack were analysed, and the corrective coefficient for the stress intensity factor was introduced. Fatigue tests with a loading frequency of f = 100 Hz were carried out on cylindrical specimens with constant amplitude of the cyclic load which is a proportion of the compressive load at failure (F f) obtained from the uni-axial compression tests. The fatigue property of the specimens was analysed and the relationship (S max − lg N f) between the maximum stress and the number of loading cycles at failure for specimens with pre-existing flaws was proposed. The effect of pre-existing flaws on the fatigue life (N f) and dynamic load (S D) which can be applied was investigated.
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Abbreviations
- a :
-
Half the flaw length (mm)
- a 0 :
-
Initial half the flaw length (mm)
- b :
-
Vertical space (mm)
- f :
-
Cyclic loading frequency (Hz)
- F f :
-
Load at failure (kN)
- F N :
-
Corrective coefficient of the stress intensity factor
- h :
-
Horizontal space (mm)
- k II :
-
Stress intensity factor for type II pure shear flaw \( \left( {{\text{MPa}}\sqrt {\text{mm}} } \right) \)
- n :
-
Number of pre-existing flaws
- N f :
-
Number of loading cycles at failure
- S D :
-
Dynamic load (kN)
- S DS :
-
Static load (kN)
- S max :
-
Maximum load (kN)
- T :
-
Test period (min)
- w :
-
Width of the specimen (mm)
- α :
-
Inclination angle of the flaw (°)
- μ f :
-
Coefficient of friction
- σ 1 :
-
Compressive stress (MPa)
- σ 1f :
-
Compressive stress at failure (MPa)
- σ α :
-
Normal stress (MPa)
- τ α :
-
Shear stress (MPa)
- τ r :
-
Resultant shear stress (MPa)
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The financial support from National Natural Science Foundation of China (10872133, 11010101024), Shanghai Pujiang Talent Program, Key Innovation Program of Shanghai Municipal Education Commission for this study is gratefully acknowledged.
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Chen, Y.L., Ni, J., Shao, W. et al. Coalescence of Fractures Under Uni-axial Compression and Fatigue Loading. Rock Mech Rock Eng 45, 241–249 (2012). https://doi.org/10.1007/s00603-011-0186-x
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DOI: https://doi.org/10.1007/s00603-011-0186-x