A Discrete Element Model for Damage and Fatigue Crack Growth of Quasi-Brittle Materials

<div>Stiffness degradation as a function of the number of cycles <svg height="11.9087pt" id="M170" style="vertical-align:-3.2728pt" version="1.1" viewbox="-0.0498162 -8.6359 14.5612 11.9087" width="14.5612pt" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink"><g transform="matrix(.013,0,0,-0.013,0,0)"><path d="M822 650H589L583 622C660 617 677 607 674 561C672 534 664 481 647 390L600 137H596L273 650H126L120 622C176 620 194 615 207 594C221 571 225 557 214 504L161 257C141 166 129 112 121 85C108 42 83 30 29 28L23 0H260L266 28C193 33 173 42 176 89C178 122 186 172 202 255L256 527H259L583 -8H612L690 390C708 481 720 535 728 558C744 603 756 619 816 622L822 650Z"></path></g><g transform="matrix(.0091,0,0,-0.0091,10.062,3.132)"><path d="M390 111C344 68 312 56 269 56C212 56 118 102 118 241C118 346 175 401 241 401C277 401 312 388 342 360C350 352 355 349 361 349C372 349 394 371 394 392C394 403 391 411 378 422C362 436 329 449 288 449H287C250 449 190 432 138 392C71 341 37 274 37 197C37 90 112 -12 238 -12C297 -12 363 32 407 90L390 111Z"></path></g></svg> for different initial crack sizes.</div>

Advances in Materials Science and Engineering

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Figure 18

Figure 18: A Discrete Element Model for Damage and Fatigue Crack Growth of Quasi-Brittle Materials 