Benchmark solution ===================== .. _RefHeading__2736_1308541645: Calculation method ----------------- The calculation of stress intensity factors is obtained in [:ref:`1 <1>`] by a semi-analytical procedure which consists in superimposing displacement profiles verifying free stress conditions on the crack lips. Reference quantities and results ----------------------------------- The values of :math:`{K}_{1}` and :math:`{K}_{2}` given in [:ref:`1 <1>`] are compared to crack bottoms. +----------+---------------+---------------++-----------------+---------------+---------------+ |**Points**|:math:`{K}_{1}`|:math:`{K}_{2}`||**Points** |:math:`{K}_{1}`|:math:`{K}_{2}`| +----------+---------------+---------------++-----------------+---------------+---------------+ |:math:`A` |1,7943 |2.8522 ||:math:`A\text{'}`|3,7215 |2.3379 | +----------+---------------+---------------++-----------------+---------------+---------------+ |:math:`B` |1,9932 |2.4042 ||:math:`B\text{'}`|2.6700 |1.0248 | +----------+---------------+---------------++-----------------+---------------+---------------+ |:math:`C` |-1.6920 |-0.1337 ||:math:`C\text{'}`|5.3966 |-0.1143 | +----------+---------------+---------------++-----------------+---------------+---------------+ |:math:`F` |0.0510 |0.2894 ||:math:`F\text{'}`|4.3255 |-0.1661 | +----------+---------------+---------------++-----------------+---------------+---------------+ |:math:`G` |-0.5317 |0.1885 ||:math:`G\text{'}`|3.6812 |0.9279 | +----------+---------------+---------------++-----------------+---------------+---------------+ |:math:`H` |-0.0517 |-0.1979 ||:math:`H\text{'}`|0.4157 |-0.3947 | +----------+---------------+---------------++-----------------+---------------+---------------+ |:math:`I` |-0.1933 |0.0213 ||:math:`I\text{'}`|1.0043 |0.0648 | +----------+---------------+---------------++-----------------+---------------+---------------+ Table 2: stress intensity factors at the bottom of cracks obtained in [:ref:`1 <1>`]. Uncertainty about the solution ---------------------------- The number of significant figures given in Table 2 reflects the quality of the semi-analytical solution. In fact, convergence towards these figures can be verified in the case of an increasingly fine mesh. Bibliographical references --------------------------- 1. A. K. YAVUZ, S. L. PHOENIX, "Multiple Crack Analysis in Finite Plates", AIAA Journal, Vol. 44, No. 11, November 2006. 2. M. SIAVELIS, M. GUITON, P. MASSIN, N. MOËS "Large sliding contact along branched discontinuities with X- FEM", under review, 2012.