| Literature DB >> 34885571 |
Youliang Chen1,2, Peng Xiao1, Xi Du1,3, Suran Wang4, Zhoulin Wang5, Rafig Azzam2.
Abstract
Based on Lemaitre's strain equivalence hypothesis theory, it is assumed that the strength of acid-etching rock microelements under the coupling effect of temperature and confining pressure follows the Weibull distribution. Under the hypothesis that micro-element damage meets the D-P criterion and based on continuum damage mechanics and statistical theory, chemical damage variables, thermal damage variables and mechanical damage variables were introduced in the construction of damage evolution equations and constitutive models for acid-etching rocks considering the coupled effects of temperature and confining pressure. The required model parameters were obtained by theoretical derivation, and the model was verified based on the triaxial compression test data of granite. Comparing the experimental stress-strain curve with the theoretical stress-strain curve, the results show that they were in good agreement. By selecting reasonable model parameters, the damage statistical constitutive model can accurately reflect the stress-strain curve characteristics of rock in the process of triaxial compression. The comparison between the experimental and theoretical results also verifies the reasonableness and reliability of the model. This model provides a new rock damage statistical constitutive equation for the study of rock mechanics and its application in engineering, and has certain reference significance for rock underground engineering.Entities:
Keywords: Weibull distribution; acid corrosion; constitutive model; coupling effect of temperature and confining pressure; damage variable; rock mechanics
Year: 2021 PMID: 34885571 PMCID: PMC8658897 DOI: 10.3390/ma14237414
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Original physical and mechanical parameters of granite under triaxial compression.
|
| ||||
|---|---|---|---|---|
| 25 | 1 | 36.43 | 0.191 | 49.68 |
| 5 | 37.30 | 0.199 | ||
| 10 | 38.70 | 0.220 | ||
| 15 | 41.10 | 0.234 | ||
| 25 | 41.80 | 0.245 | ||
| 200 | 1 | 35.55 | 0.212 | 48.96 |
| 5 | 38.14 | 0.243 | ||
| 10 | 39.30 | 0.268 | ||
| 15 | 42.12 | 0.283 | ||
| 25 | 42.83 | 0.297 | ||
| 400 | 1 | 30.40 | 0.240 | 51.89 |
| 5 | 33.60 | 0.274 | ||
| 10 | 37.36 | 0.311 | ||
| 15 | 39.05 | 0.327 | ||
| 25 | 40.46 | 0.343 | ||
| 600 | 1 | 21.09 | 0.255 | 51.48 |
| 5 | 26.94 | 0.282 | ||
| 10 | 28.52 | 0.309 | ||
| 15 | 31.36 | 0.336 | ||
| 25 | 34.13 | 0.352 | ||
| 800 | 1 | 13.57 | 0.264 | 46.83 |
| 5 | 17.79 | 0.302 | ||
| 10 | 21.43 | 0.332 | ||
| 15 | 23.51 | 0.340 | ||
| 25 | 27.73 | 0.376 |
Model calculation parameters of triaxial compression of granite.
|
| |||||
|---|---|---|---|---|---|
| 25 | 1 | 134.02 | 0.520 | 2.901 | 222.591 |
| 5 | 168.50 | 0.611 | 3.362 | 270.240 | |
| 10 | 221.16 | 0.694 | 5.266 | 308.440 | |
| 15 | 267.10 | 0.805 | 4.797 | 387.323 | |
| 25 | 308.19 | 0.887 | 5.614 | 433.885 | |
| 200 | 1 | 143.00 | 0.560 | 3.033 | 232.974 |
| 5 | 178.32 | 0.640 | 3.224 | 289.190 | |
| 10 | 230.00 | 0.745 | 4.217 | 343.619 | |
| 15 | 274.40 | 0.819 | 4.462 | 405.912 | |
| 25 | 310.91 | 0.908 | 4.599 | 464.908 | |
| 400 | 1 | 104.00 | 0.550 | 2.115 | 195.730 |
| 5 | 147.00 | 0.670 | 2.376 | 270.941 | |
| 10 | 205.00 | 0.716 | 3.819 | 322.005 | |
| 15 | 245.00 | 0.821 | 3.787 | 389.997 | |
| 25 | 305.00 | 0.909 | 5.468 | 437.147 | |
| 600 | 1 | 82.14 | 0.647 | 1.979 | 158.301 |
| 5 | 135.00 | 0.775 | 2.323 | 251.071 | |
| 10 | 170.00 | 0.840 | 2.971 | 294.258 | |
| 15 | 200.00 | 0.881 | 3.160 | 343.006 | |
| 25 | 287.78 | 1.050 | 4.664 | 434.994 | |
| 800 | 1 | 68.05 | 0.883 | 1.777 | 133.929 |
| 5 | 104.00 | 0.958 | 2.055 | 200.243 | |
| 10 | 140.00 | 1.030 | 2.239 | 266.396 | |
| 15 | 166.83 | 1.110 | 2.287 | 319.621 | |
| 25 | 225.00 | 1.228 | 2.468 | 426.229 |
Peak values of stress-strain test curves and theoretical curves of granite under different temperatures and confining pressures.
|
|
| R | ||||
|---|---|---|---|---|---|---|
| 25 | 1 | 134.02 | 0.520 | 134.00 | 0.528 | 0.998 |
| 5 | 168.50 | 0.611 | 168.50 | 0.616 | ||
| 10 | 221.16 | 0.694 | 221.00 | 0.704 | ||
| 15 | 267.10 | 0.805 | 267.10 | 0.802 | ||
| 25 | 308.19 | 0.887 | 308.20 | 0.905 | ||
| 200 | 1 | 143.00 | 0.560 | 142.90 | 0.572 | 0.999 |
| 5 | 178.32 | 0.640 | 178.30 | 0.641 | ||
| 10 | 230.00 | 0.745 | 229.90 | 0.752 | ||
| 15 | 274.40 | 0.819 | 274.30 | 0.818 | ||
| 25 | 310.91 | 0.908 | 310.80 | 0.916 | ||
| 400 | 1 | 104.00 | 0.550 | 104.00 | 0.549 | 0.998 |
| 5 | 147.00 | 0.670 | 147.00 | 0.669 | ||
| 10 | 205.00 | 0.716 | 205.00 | 0.723 | ||
| 15 | 245.00 | 0.821 | 245.00 | 0.828 | ||
| 25 | 305.00 | 0.909 | 305.00 | 0.912 | ||
| 600 | 1 | 82.14 | 0.647 | 82.15 | 0.645 | 0.999 |
| 5 | 135.00 | 0.775 | 135.00 | 0.778 | ||
| 10 | 170.00 | 0.840 | 170.10 | 0.841 | ||
| 15 | 200.00 | 0.881 | 200.00 | 0.885 | ||
| 25 | 287.78 | 1.050 | 287.90 | 1.050 | ||
| 800 | 1 | 68.05 | 0.883 | 68.06 | 0.891 | 0.997 |
| 5 | 104.00 | 0.958 | 104.00 | 0.943 | ||
| 10 | 140.00 | 1.030 | 140.00 | 1.030 | ||
| 15 | 166.83 | 1.110 | 166.80 | 1.098 | ||
| 25 | 225.00 | 1.228 | 225.00 | 1.232 |
Figure 1Experimental and theoretical stress-strain curves under different confining pressures. (a) 1 Mpa; (b) 5 Mpa; (c) 10 Mpa; (d) 15 Mpa; (e) 25 Mpa.
Figure 2Experimental and theoretical stress-strain curves at different temperatures. (a) 25 °C; (b) 200 °C; (c) 400 °C; (d) 600 °C; (e) 800 °C.