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