fastoad_cs25.models.geometry.geom_components.ht.ht_global_positions module

Convenience module for computing leading edge X positions of wing chords.

class fastoad_cs25.models.geometry.geom_components.ht.ht_global_positions.HTChordGlobalPositions(**kwargs)

Bases: Group

Computes leading edge X positions of horizontal tail chords (root, tip) with respect to aircraft nose.

Set the solvers to nonlinear and linear block Gauss–Seidel by default.

setup()

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 fastoad_cs25.models.geometry.geom_components.ht.ht_global_positions.ComputeChordGlobalPositions(**kwargs)

Bases: Group

Computes leading edge X positions of horizontal tail chords with respect to aircraft nose.

Set the solvers to nonlinear and linear block Gauss–Seidel by default.

setup()

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