fastga.models.weight.mass_breakdown.a_airframe.a1_wing_weight_analytical module

Python module for wing weight calculation using the analytical breakdown. Based on the model presented by Raquel ALONSO in her MAE research project report. [ACLJezegouBenard21]

class fastga.models.weight.mass_breakdown.a_airframe.a1_wing_weight_analytical.ComputeWingMassAnalytical(**kwargs)

Bases: openmdao.core.group.Group

Computes analytically the mass of each component of the wing and add them to get total wing mass

Loop on the wing mass cause its both a relief force and the result.

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