C-D === .. csv-table:: "**Option_name**", "**Purpose**", "**Phenomena**", "**Domain**" "CALC_ESTI_ERRE ", "Calculation of the error estimator in element-wise energy norm, at Gauss points", "mechanics", "Post-processing" "CALC_G ", "Calculation of the energy return rate", "mechanics", "Mechanics of rupture" "CALC_G_F ", "Calculation of the energy return rate (with input functions)", "mechanics", "Mechanics of rupture" "CALC_G_GLOB ", "Calculation of the global energy restoration rate in 3D over the entire crack front", "mechanics", "Fracture mechanics" "CALC_G_GLOB_F ", "Calculation of the global energy restoration rate in 3D over the entire crack front (with input functions)", "mechanics", "Fracture mechanics" "CALC_K_G ", "Calculation of stress intensity factors at the bottom of a crack using G", "mechanics", "Fracture mechanics" "CALC_K_G_F ", "Calculation of stress intensity factors at the bottom of a crack using G (with input functions)", "mechanics", "Fracture mechanics" "CALC_NOEU_BORD ", "Calculation of the elementary vector normal to the edge at the nodes (in 2D)", "", "" "CARA_CISA ", "Calculation of the transverse shear characteristics of a 2D beam section", "thermal", "Post-treatment" "CARA_GAUCHI ", "Calculation of warping characteristics of a 2D beam section", "thermal", "Post-treatment" "CARA_GEOM ", "Calculation of the geometric characteristics of a 2D section of a beam: inertia", "mechanics", "" "CARA_SECT_POU3R ", "Calculation for the elem_link", "mechanics", "Loads" "CARA_SECT_POUT3 ", "Calculation of the elementary field with 10 components sum/S_element (DS, X.DS, S.DS, Y.DS, Z.DS, X*Y.DS, Z*Z.DS, X*Y.DS, X*Y.DS, X*Z.DS, X*Z.DS, X*Z.DS) on faces of 3D isoparametric elements (for the link_elem)", "mechanics", "Loads" "CARA_SECT_POUT4 ", "Calculation of the 2 vectors defined at the nodes of the elements whose values at node Ide the element are: for the first vector sum/s_element (NI.DS,0,0) and for the second vector sum/s_element (X*NI.DS, Y*NI.DS, Y*NI.DS, Z*NI.DS) on faces of 3D isoparametric elements (for the link_elem)", "mechanics", "Loadings" "CARA_SECT_POUT5 ", "Calculation of the vector defined at the nodes of the elements whose values are at node I of the sum/s_element (NI) element (NI). COS (M. PHI) .P.DS) on faces of 3D isoparametric elements. For the 3D_Pipe_Pipe_and Coque_Tube_Connector connection. ", "mechanics", "Loads" "CARA_TORSION ", "Calculation of the torsional characteristics of a 2D beam section", "thermal", "Post-treatment" "CFL_XFEM ", "Calculation of conditions CFL; elementary field calculations (delta_phi) necessary for the reset and reorthogonalization phases (XFEMet propagation method)", "mechanical", " "CHAR_ACOU_VNOR_C ", "Calculation of elementary vectors corresponding to the normal velocities imposed on the faces of isoparametric elements", "acoustics", "Loads" "CHAR_DLAG_EVOLST ", "Calculation of the elementary vectors corresponding to the terms from the Lagrangian derivation (theta method) of the first member of the stationary equation", "thermal", "Loads; Mechanics of rupture" "CHAR_DLAG_EVOLTR ", "Calculation of the elementary vectors corresponding to the terms from the Lagrangian derivation (theta method) of the first member of the transient equation", "thermal", "Loads; Mechanics of rupture" "CHAR_DLAG_FLUN_F ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of heat flows (with input functions)", "thermal", "Loads; Mechanics of rupture" "CHAR_DLAG_FLUN_R ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of heat flows", "thermal", "Loads; Mechanics of rupture" "CHAR_DLAG_MECAST ", "Calculation of the elementary vectors corresponding to the terms from the Lagrangian derivation (theta method) of the first member of the equation", "mechanics", "Loads; Mechanics of rupture" "CHAR_DLAG_PRES_F ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of surface pressure loading (with input functions)", "mechanics", "Loads", "Loads; Fracture mechanics" "CHAR_DLAG_PRES_R ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of surface pressure loading", "mechanics", "Loads; Fracture mechanics" "CHAR_DLAG_SOUR_F ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of the thermal volume source (with input functions)", "thermal", "Loads", "Loads; Fracture mechanics" "CHAR_DLAG_SOUR_R ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of the thermal volume source", "thermal", "Loads; Mechanics of rupture" "CHAR_DLAG_TEXT_F ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of the outside temperature (with input functions)", "thermal", "Loads; Mechanics of rupture" "CHAR_DLAG_TEXT_R ", "Calculation of the elementary vectors corresponding to the terms coming from the Lagrangian derivation (theta method) of the outside temperature", "thermal", "Loads; Mechanics of rupture" "CHAR_LIMITE ", "Calculation of elementary terms for the limit load on incompressible elements", "mechanics", "Post-processing; Nonlinear calculation" "CHAR_LIMITE_F ", "Calculation of elementary terms for the limit load on incompressible elements", "mechanics", "Post-processing; Nonlinear calculation" "CHAR_MECA_CONT ", "Calculation of the second elementary contact member with the continuous ECP method ", "Mechanics", "Loads; Nonlinear calculation" "CHAR_MECA_EPSA_R ", "Calculation of the second elementary member corresponding to anelastic deformations (keyword: epsa_calculus)", "mechanics", "Loads" "CHAR_MECA_EPSI_F ", "Calculation of the second elementary member corresponding to initial deformations (with input functions)", "mechanics", "Loads" "CHAR_MECA_EPSI_R ", "Calculation of the second elementary member corresponding to initial deformations", "mechanics", "Loads" "CHAR_MECA_FC1D1D ", "Calculation of the second elementary member corresponding to complex linear forces (keyword: force_beam)", "mechanics", "Loads" "CHAR_MECA_FF1D1D ", "Calculation of the second elementary member corresponding to linear forces applied along a beam (with input functions)", "mechanics", "Loads" "CHAR_MECA_FF1D2D ", "Calculation of the second elementary member corresponding to linear forces applied to an edge of a 2D domain (with input functions)", "mechanics", "Loads" "CHAR_MECA_FF1D3D ", "Calculation of the second elementary member corresponding to linear forces applied to an edge of a 3D domain (with input functions)", "mechanics", "Loads" "CHAR_MECA_FF2D2D ", "Calculation of the second elementary member corresponding to internal forces applied to a 2D domain (with input functions)", "mechanics", "Loads" "CHAR_MECA_FF2D3D ", "Calculation of the second elementary member corresponding to surface forces applied to a face of a 3D domain (with input functions)", "mechanics", "Loads" "CHAR_MECA_FF3D3D ", "Calculation of the second elementary member corresponding to internal forces applied to a 3D domain (with input functions)", "mechanics", "Loads" "CHAR_MECA_FFCO2D ", "Calculation of the second elementary member corresponding to surface forces applied to a shell_1D element (keyword: shell_force) (with input functions)", "mechanics", "Loads" "CHAR_MECA_FFCO3D ", "Calculation of the second elementary member corresponding to surface forces applied to a shell element (keyword: force_shell) (with input functions)", "mechanics", "Loads" "CHAR_MECA_FLUX_F ", "Calculation of the second elementary member corresponding to a flow THMréparti (with input functions)", "mechanics", "Loads" "CHAR_MECA_FLUX_R ", "Calculation of the second elementary member corresponding to a flow THMréparti ", "mechanical", "Loads" "CHAR_MECA_FORC_F ", "Calculation of the second elementary member corresponding to nodal forces (with input functions)", "mechanics", "Loads" "CHAR_MECA_FORC_R ", "Calculation of the second elementary member corresponding to nodal forces", "mechanics", "Loads" "CHAR_MECA_FR1D1D ", "Calculation of the second elementary member corresponding to linear forces applied along a beam", "mechanics", "Loads" "CHAR_MECA_FR1D2D ", "Calculation of the second elementary member corresponding to linear forces applied to an edge of a 2D domain", "mechanics", "Loads" "CHAR_MECA_FR1D3D ", "Calculation of the second elementary member corresponding to linear forces applied to an edge of a 3D domain", "mechanics", "Loads" "CHAR_MECA_FR2D2D ", "Calculation of the second elementary member corresponding to internal forces applied to a 2D domain", "mechanics", "Loads" "CHAR_MECA_FR2D3D ", "Calculation of the second elementary member corresponding to surface forces applied to a face of a 3D domain", "mechanics", "Loads" "CHAR_MECA_FR3D3D ", "Calculation of the second elementary member corresponding to internal forces applied to a 3D domain", "mechanics", "Loads" "CHAR_MECA_FRCO2D ", "Calculation of the second elementary member corresponding to surface forces applied to shell_1D elements (keyword: shell_force)", "mechanics", "Loads" "CHAR_MECA_FRCO3D ", "Calculation of the second elementary member corresponding to surface forces applied to shell elements (keyword: shell_force)", "mechanics", "Loads" "CHAR_MECA_FRELEC ", "Calculation of the second elementary member corresponding to an electrical force (keyword FORC_ELEC)", "mechanics", "Loads" "CHAR_MECA_FRLAPL ", "Calculation of the second elementary member corresponding to Laplace forces (keyword inte_elec)", "mechanics", "Loads" "CHAR_MECA_FROT ", "Calculation of the second elementary member of standard friction with the ECP continuous method (keyword: contact)", "mechanics", "Loads" "CHAR_MECA_HYDR_R ", "Calculation of the second elementary member corresponding to a hydration and temperature field (keyword: hydr_calculus)", "mechanics", "Loads" "CHAR_MECA_META_Z ", "Te0353/358", "mechanics", "Loads" "CHAR_MECA_ONDE ", "(MOT - CLE: ONDE_FLUI): Calculation of the second elementary member corresponding to a pressure D' ONDE INCIDENTE SINUSOIDALE ARRIVANT NORMALEMENT A LA FACE ", "mechanics", "Loads" "CHAR_MECA_PESA_R ", "Calculation of the second elementary member corresponding to gravity", "mechanics", "Loads" "CHAR_MECA_PRES_F ", "Calculation of the second elementary member corresponding to a surface pressure (with input functions)", "mechanics", "Loads" "CHAR_MECA_PRES_R ", "Calculation of the second elementary member corresponding to a surface pressure", "mechanics", "Loads" "CHAR_MECA_PRSU_F ", "Calculation of the second elementary member corresponding to a surface force (with input functions)", "mechanics", "Loads" "CHAR_MECA_PRSU_R ", "Calculation of the second elementary member corresponding to a surface force", "mechanics", "Loads" "CHAR_MECA_ROTA_R ", "Calculation of the second elementary member from rotational drive accelerations", "mechanics", "Loads" "CHAR_MECA_SECH_R ", "Calculation of the second elementary member from deformations due to drying", "mechanics", "Loads" "CHAR_MECA_SF1D1D ", "Calculation of the second elementary member for a beam", "mechanics", "Loads" "CHAR_MECA_SFCO3D ", "Calculation of the second elementary member for a shell", "mechanics", "Loads" "CHAR_MECA_SR1D1D ", "Calculation of the second elementary member for a beam", "mechanics", "Loads" "CHAR_MECA_SRCO3D ", "Calculation of the second elementary member for a shell", "mechanics", "Loads" "CHAR_MECA_TEMP_R ", "Calculation of the second elementary member from thermal deformations", "mechanics", "Loads" "CHAR_MECA_VNOR ", "Calculation of the second elementary member coming from a normal speed imposed on an edge of a fluid domain in 2D and 3D", "mechanics", "Loads" "CHAR_MECA_VNOR_F ", "Calculation of the second elementary member coming from a normal speed imposed on an edge of a fluid domain in 2D and 3D (with input functions)", "mechanics", "Loads" "CHAR_THER_ACCE_R ", "", "thermal", "" "CHAR_THER_ACCE_X ", "", "thermal", "" "CHAR_THER_ACCE_Y ", "", "thermal", "" "CHAR_THER_ACCE_Z ", "", "thermal", "" "CHAR_THER_EVOL ", "", "thermal", "" "CHAR_THER_EVOLNI ", "", "thermal", "" "CHAR_THER_FLUN_F ", "", "thermal", "Loads" "CHAR_THER_FLUN_R ", "", "thermal", "Loads" "CHAR_THER_FLUNL ", "", "thermal", "Loads" "CHAR_THER_FLUTNL ", "", "thermal", "Loads" "CHAR_THER_FLUX_F ", "", "thermal", "Loads" "CHAR_THER_FLUX_R ", "", "thermal", "Loads" "CHAR_THER_GRAI_F ", "", "thermal", "" "CHAR_THER_GRAI_R ", "", "thermal", "" "CHAR_THER_PARO_F ", "", "thermal", "" "CHAR_THER_PARO_R ", "", "thermal", "" "CHAR_THER_PHID_R ", "", "thermal", "" "CHAR_THER_RAYO_F ", "", "thermal", "" "CHAR_THER_RAYO_R ", "", "thermal", "" "CHAR_THER_SOUR_F ", "", "thermal", "Loads" "CHAR_THER_SOUR_R ", "", "thermal", "Loads" "CHAR_THER_TEXT_F ", "", "thermal", "Loads" "CHAR_THER_TEXT_R ", "", "thermal", "Loads" "CHAR_THER_TNL ", "", "thermal", "" "COOR_ELGA ", "Coordinates from Gauss points to Gauss points", "", ""