fastga.models.geometry.geom_components.fuselage.compute_fuselage module
Python module for fuselage geometry calculation - Cabin (Commercial), part of the geometry component.
- class fastga.models.geometry.geom_components.fuselage.compute_fuselage.ComputeFuselageAlternate(**kwargs)[source]
Bases:
openmdao.core.group.GroupFuselage geometry calculations with fixed rear fuselage length cabin sizing.
Set the solvers to nonlinear and linear block Gauss–Seidel by default.
- setup()[source]
Build this group.
This method should be overidden by your Group’s method. The reason for using this method to add subsystem is to save memory and setup time when using your Group while running under MPI. This avoids the creation of systems that will not be used in the current process.
You may call ‘add_subsystem’ to add systems to this group. You may also issue connections, and set the linear and nonlinear solvers for this group level. You cannot safely change anything on children systems; use the ‘configure’ method instead.
- Available attributes:
name pathname comm options
- class fastga.models.geometry.geom_components.fuselage.compute_fuselage.ComputeFuselageLegacy(**kwargs)[source]
Bases:
openmdao.core.group.GroupFuselage geometry calculations with fixed MACs distance cabin sizing.
Set the solvers to nonlinear and linear block Gauss–Seidel by default.
- setup()[source]
Build this group.
This method should be overidden by your Group’s method. The reason for using this method to add subsystem is to save memory and setup time when using your Group while running under MPI. This avoids the creation of systems that will not be used in the current process.
You may call ‘add_subsystem’ to add systems to this group. You may also issue connections, and set the linear and nonlinear solvers for this group level. You cannot safely change anything on children systems; use the ‘configure’ method instead.
- Available attributes:
name pathname comm options