Modeling A ============== Characteristics of modeling ----------------------------------- The entire test piece is meshed into quadrangular elements with 4 knots or triangular elements with 3 knots. It has 799 nodes, 624 quadrangles, 185 triangles, and 261 segments. Characteristics of the mesh ---------------------------- Very small elements (:math:`\mathrm{0,02}\mathrm{mm}`) at the tip of the crack. The first ring is located in a single material, the 4 other rings cross the interface between the two materials. .. image:: images/100041CA00002E6800002BED034B05B8F3BDF5A4.svg :width: 598 :height: 566 .. _RefImage_100041CA00002E6800002BED034B05B8F3BDF5A4.svg: .. image:: images/10000000000001C90000013DAF6A1894698B8CC3.png :width: 625 :height: 414 .. _RefImage_10000000000001C90000013DAF6A1894698B8CC3.png: .. image:: images/1000410C00003393000022361F217C689A3DD090.svg :width: 598 :height: 566 .. _RefImage_1000410C00003393000022361F217C689A3DD090.svg: Tested sizes and results ------------------------------ The energy return rate :math:`G` is calculated by the :math:`\mathrm{THETA}` method for the following 5 crowns: * Crown 0: :math:`{R}_{\mathrm{inf}}=\mathrm{0,02}\mathrm{mm}` :math:`{R}_{\text{supĀ }}=\mathrm{0,18}\mathrm{mm}` * Crown 1: :math:`{R}_{\mathrm{inf}}=\mathrm{0,2}\mathrm{mm}` :math:`{R}_{\text{sup}}=1\mathrm{mm}` * Crown 2: :math:`{R}_{\mathrm{inf}}=1\mathrm{mm}` :math:`{R}_{\text{sup}}=2\mathrm{mm}` * Crown 3: :math:`{R}_{\mathrm{inf}}=2\mathrm{mm}` :math:`{R}_{\text{sup}}=3\mathrm{mm}` * Crown 4: :math:`{R}_{\mathrm{inf}}=3\mathrm{mm}` :math:`{R}_{\text{sup}}=5\mathrm{mm}` Tested values .. csv-table:: "**Identification**", "**Reference** **J ASTM**", "**Aster**", ":math:`\text{\%}` **difference**" "G (N/mm) Crown No. 0 UY=0.2 mm", "5.8", "6.0", "3.1" "G (N/mm) Crown No. 0 UY=0.4 mm", "22.6", "23.2", "2.8" "G (N/mm) Crown No. 0 UY=0.6 mm", "47.2", "48.2", "2.0" "G (N/mm) Crown No. 0 UY=0.8 mm", "74.7", "75.0", "0.5" "G (N/mm) Crown No. 0 UY=1.0 mm", "103.7", "102.8", "-0.8" "", "", "", "" "G (N/mm) Crown #1 UY=0.2 mm", "5.8", "6.10", "4.6" "G (N/mm) Crown #1 UY=0.4 mm", "22.6", "23.2", "2.8" "G (N/mm) Crown #1 UY=0.6 mm", "47.2", "47.3", "0.1" "G (N/mm) Crown #1 UY=0.8mm", "74.7", "73.1", "2.2" "G (N/mm) Crown #1 UY=1.0mm", "103.7", "99.8", "3.8" "", "", "", "" "G (N/mm) Crown #2 UY=0.2 mm", "5.8", "6.1", "4.3" "G (N/mm) Crown #2 UY=0.4 mm", "22.6", "23.3", "3.2" "G (N/mm) Crown #2 UY=0.6 mm", "47.2", "48.0", "1.6" "G (N/mm) Crown #2 UY=0.8mm", "74.7", "74.9", "0.3" "G (N/mm) Crown #2 UY=1.0 mm", "103.7", "103.7", "103.1", "0.3" .. csv-table:: "**Identification**", "**Reference** **J ASTM**", "**Aster**", ":math:`\text{\%}` **difference**" "G (N/mm) Crown #3 UY=0.2 mm", "5.8", "6.1", "4.4" "G (N/mm) Crown #3 UY=0.4 mm", "22.6", "23.3", "3.3" "G (N/mm) Crown #3 UY=0.6 mm", "47.2", "48.2", "1.9" "G (N/mm) Crown #3 UY=0.8mm", "74.7", "75.5", "1.0" "G (N/mm) Crown #3 UY=1.0 mm", "103.7", "104.2", "0.4" "", "", "", "" "G (N/mm) Crown No. 4 UY=0.2 mm", "5.8", "6.1", "4.5" "G (N/mm) Crown No. 4 UY=0.4 mm", "22.6", "23.4", "3.4" "G (N/mm) Crown No. 4 UY=0.6 mm", "47.2", "48.2", "2.1" "G (N/mm) Crown #4 UY=0.8mm", "74.7", "75.5", "1.1" "G (N/mm) Crown #4 UY=1.0 mm", "103.7", "104.4", "0.7" **Stability of** :math:`G` **with the choice of crowns** .. csv-table:: "**Identification**", "**Crown 2**", "**Crown 3**", "**Crown 4**", ":math:`\text{\%}` **Maximum variance**" "G (N/mm) UY=0.2mm", "6.1", "6.1", "6.1", "6.1", "0.2" "G (N/mm) UY=0.4mm", "23.3", "23.3", "23.4", "0.1" "G (N/mm) UY=0.6mm", "48.0", "48.2", "48.2", "0.4" "G (N/mm) UY=0.8mm", "74.9", "75.5", "75.5", "0.5" "G (N/mm) UY=1.0mm", "103.1", "103.1", "104.2", "104.4", "0.4" notes --------- In all cases, the absolute value of the difference in the calculation of :math:`G` is less than :math:`\text{5\%}`. For rings 3 to 5, the difference decreases as a function of the displacement to reach an almost zero value. The stability on rings 2, 3 and 4 is very good, the gap between rings is always less than :math:`\text{0,5 \%}`.