NUMBER: 1 CONDITION: Apply_constraint_on_points CONDTYPE: over points CONDMESHTYPE: over nodes QUESTION: with_respect_to#CB#(-Global_axes-,-Local_axes-) VALUE: -Global_axes- HELP: CAUTION: local axes constraints are not implemented yet QUESTION: Ux#CB#(1,0) VALUE: 0 HELP: if this condition is marked the corresponding DOF will be restrained QUESTION: Uy#CB#(1,0) VALUE: 0 HELP: if this condition is marked the corresponding DOF will be restrained QUESTION: Uz#CB#(1,0) VALUE: 0 HELP: if this condition is marked the corresponding DOF will be restrained QUESTION: theta_x#CB#(1,0) VALUE: 0 HELP: if this condition is marked the corresponding DOF will be restrained QUESTION: theta_y#CB#(1,0) VALUE: 0 HELP: if this condition is marked the corresponding DOF will be restrained QUESTION: theta_z#CB#(1,0) VALUE: 0 HELP: if this condition is marked the corresponding DOF will be restrained QUESTION: warping_intensity#CB#(1,0) VALUE: 0 HELP: if this condition is marked the corresponding DOF will be restrained END CONDITION NUMBER: 2 CONDITION: assign_cross_section CONDTYPE: over lines CONDMESHTYPE: over body elements QUESTION: cross_section_number VALUE: 1 HELP: the cross-section numbers must be in ascending consecutive order, starting with 1 QUESTION: section_type#CB#(vlasov_elastic_rod_section,vlasov_st_venant_elastic_rod_section,vlasov_simo_elastic_rod_section) VALUE: vlasov_elastic_rod_section HELP: CAUTION! The section type must agree with the type of material assigned to the line(s). QUESTION: A VALUE: 0.0 QUESTION: I11 VALUE: 0.0 HELP: Flexural Inertia I11; value must be with respect to the local system defined for this line or element QUESTION: I22 VALUE: 0.0 HELP: Flexural Inertia I22; value must be with respect to the local system defined for this line or element QUESTION: It VALUE: 0.0 HELP: Torsional Inertia It; value must be with respect to the local system defined for this line or element QUESTION: I12 VALUE: 0.0 HELP: Product of Inertia I12; value must be with respect to the local system defined for this line or element QUESTION: G1 VALUE: 0.0 HELP: Coordinate 1 of the section centroid; value must be with respect to the local system defined for this line or element QUESTION: G2 VALUE: 0.0 HELP: Coordinate 2 of the section centroid; value must be with respect to the local system defined for this line or element QUESTION: S1 VALUE: 0.0 HELP: Coordinate 1 of the shear center; value must be with respect to the local system defined for this line or element QUESTION: S2 VALUE: 0.0 HELP: Coordinate 2 of the shear center; value must be with respect to the local system defined for this line or element QUESTION: Iw VALUE: 0.0 HELP: Warping inertia Iw; value must be with respect to the local system defined for this line or element END CONDITION NUMBER: 3 CONDITION: apply_concentrated_load CONDTYPE: over points CONDMESHTYPE: over nodes QUESTION: with_respect_to#CB#(-Global_axes-,-Local_axes-) VALUE: -Global_axes- HELP: CAUTION: local axes loads are not implemented yet QUESTION: Fx VALUE: 0.0 QUESTION: Fy VALUE: 0.0 QUESTION: Fz VALUE:0.0 QUESTION: Mx VALUE: 0.0 QUESTION: My VALUE: 0.0 QUESTION: Mz VALUE: 0.0 QUESTION: B VALUE: 0.0 HELP: Nodal (concentrated) bi-moment END CONDITION NUMBER: 4 CONDITION: apply_distributed_load CONDTYPE: over lines CONDMESHTYPE: over body elements QUESTION: with_respect_to#CB#(-Global_axes-,-Local_axes-) VALUE: -Global_axes- HELP: CAUTION: local axes loads are not implemented yet QUESTION: qx VALUE: 0.0 QUESTION: qy VALUE: 0.0 QUESTION: qz VALUE:0.0 QUESTION: mx VALUE: 0.0 QUESTION: my VALUE: 0.0 QUESTION: mz VALUE: 0.0 QUESTION: b VALUE: 0.0 HELP: Uniformly distributed bi-moment END CONDITION NUMBER: 5 CONDITION: assign_local_system CONDTYPE: over lines CONDMESHTYPE: over body elements QUESTION: local_system_number VALUE: 1 HELP: the local system numbers must be in ascending consecutive order, starting with 1 QUESTION: local_system_name#CB#(vlasov_rod_local_system) VALUE: vlasov_rod_local_system HELP: CAUTION! The local system name must agree with the type of element assigned to the line(s). One should be very careful when assigning the local system vector: PEFSYS defines the local axis 3 as the vector that points from node "i" to node "j" of the element. Then axis 2 is defined as being the result of the vector product between axis 3 and the local system vector. Then axis 1 is the vector product between axis 2 and axis 3. QUESTION: loc_sys_vector_component_1 VALUE: 1.0 HELP: This is the component 1 of the vector that defines the local system (value must be with respect to the global system). One should be very careful when assigning the local system vector: PEFSYS defines the local axis 3 as the vector that points from node "i" to node "j" of the element. Then axis 2 is defined as being the result of the vector product between axis 3 and the local system vector. Then axis 1 is the vector product between axis 2 and axis 3. QUESTION: loc_sys_vector_component_2 VALUE: 0.0 HELP: This is the component 2 of the vector that defines the local system (value must be with respect to the global system). One should be very careful when assigning the local system vector: PEFSYS defines the local axis 3 as the vector that points from node "i" to node "j" of the element. Then axis 2 is defined as being the result of the vector product between axis 3 and the local system vector. Then axis 1 is the vector product between axis 2 and axis 3. QUESTION: loc_sys_vector_component_3 VALUE: 0.0 HELP: This is the component 3 of the vector that defines the local system (value must be with respect to the global system). One should be very careful when assigning the local system vector: PEFSYS defines the local axis 3 as the vector that points from node "i" to node "j" of the element. Then axis 2 is defined as being the result of the vector product between axis 3 and the local system vector. Then axis 1 is the vector product between axis 2 and axis 3. END CONDITION