====== BLZ2D ====== FIXME The prepro subroutine for BLZ2D seems to have been copy/pasted from [[elements:blz3d|BLZ3D]] and contains discrepancies (notably NNODE = 8 when NNODE should be = 4) \\ The prepro subroutine needs to be checked and corrected. ===== Description ===== Plane or axisymmetric state. \\ For the axisymmetric state, the symmetry axis is Y. The element is defined by 4 nodes. {{ :elements:plani.png?200|}} \\ Element type: 8 \\ Revised by: Y. Zhu (1991) ==== Files ==== Prepro: BLZ2DA.F \\ Lagamine: BLZ2DB.F ===== Input file ===== **Note**: The prepro subroutine for BLZ2D seems to have been copy/pasted from [[elements:blz3d|BLZ3D]]. However, it is highly uncertain that all the features available for BLZ3D are as well available for BLZ2D. The uncertain features are written below in italic. ^Title (A5)^^ |TITLE|"BLZ2D" in columns 1 to 5| ^ Control data (2I5) ^^ |NELEM| Number of elements | |INDPP| 0 → Static \\ 1 → Dynamic| |INSHE|= 0 for automatic calculation of shear locking parameter| |::: |//= 1 if shear coefficient taken into account//| |//ILOAX//|//= 0 for global axis computation \\ ☛ Objectivity must be verified in the material law (with Jaumann correction)\\ ☛ No rotation of material axes//| |:::|//< 0 for computation with constant and symetrical velocity gradients \\ pseudo local axes : use of local axes on the time step but no evolution of the local axes on the following time step \\ ☛ Objectivity is verified \\ ☛ No rotation of material axes//| |:::|//> 0 for computation with local axes \\ ☛ Objectivity is verified \\ ☛ Rotation of material axes//| |:::|//units: \\ = 1 for rotations incorporated in local tangent matrix :!: **Not available** \\ = 2 apply final rotation to local tangent matrix \\ = 3 apply initial rotation to local tangent matrix \\ = 4 compute tangent matrix through global perturbation method//| |:::|//tens (only for ILOAX>0): \\ = 0 for local axes e1, e2, e3 initially parallel to global axes ex, ey, ez \\ = 1 for local axes e1, e2 given (and e3=e1∧e2) \\ = 2 for local axes e1, e2 initially in the plane (ex, ey) forming an angle θ with ex, ey (and e3=e1∧e2)\\ = 3 same as 1 with different local axes for each element \\ = 4 same as 2 with different local axes for each element//| |INSIG| 0 → No initial stresses \\ 1 → $\sigma_Y=\sigma_{Y0}+yd\sigma_Y$ \\ 3 → See [[elements:plxls|PLXLS]]| ^Specific weight - Only if INDPP = 1 (3G10.0)^^ |WSPE(1)| = specific weight in X direction| |WSPE(2)| = specific weight in Y direction| |WSPE(3)| = density| ^//Shear coefficient - Only if INSHE > 0 (G10.0)//^^ |//PARSHE//| //Shear locking coefficient ∈ [0,1] \\ - close to 0: avoid shear locking but higher risk of hourglass modes (use for thin elements in flexion) \\ - close to 1: avoid hourglass modes but higher risk of shear locking (use for cubic elements in shear)//| ^Definition of the elements (2I5/4I5) ^^ |NINTE| Number of integration points (1, 2, or 4)| |LMATE| Number of the material law| |NODES(4)| List of nodes| |SIG0(6)| List of initial stresses (Only if INSIG ≠ 0) \\ **If INSIG = 1 (3G10.0)**: \\ $\sigma_{Y0}$ - Effective stress $\sigma_Y$ at the axes origin \\ DSIGY - Gradient of effective stress along axis OY \\ AK0 - ratio $\sigma_X/\sigma_Y$ \\ **If INSIG = 3 (6G10.0)**: See [[elements:plxls|PLXLS]]|