"""
Estimation of wing geometry
"""
# This file is part of FAST-OAD : A framework for rapid Overall Aircraft Design
# Copyright (C) 2020 ONERA & ISAE-SUPAERO
# FAST is free software: you can redistribute it and/or modify
# it under the terms of the GNU General Public License as published by
# the Free Software Foundation, either version 3 of the License, or
# (at your option) any later version.
# This program is distributed in the hope that it will be useful,
# but WITHOUT ANY WARRANTY; without even the implied warranty of
# MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the
# GNU General Public License for more details.
# You should have received a copy of the GNU General Public License
# along with this program. If not, see <https://www.gnu.org/licenses/>.
from openmdao.api import Group
from fastoad.models.geometry.geom_components.wing.components.compute_b_50 import ComputeB50
from fastoad.models.geometry.geom_components.wing.components.compute_cl_alpha import ComputeCLalpha
from fastoad.models.geometry.geom_components.wing.components.compute_l1_l4 import ComputeL1AndL4Wing
from fastoad.models.geometry.geom_components.wing.components.compute_l2_l3 import ComputeL2AndL3Wing
from fastoad.models.geometry.geom_components.wing.components.compute_mac_wing import ComputeMACWing
from fastoad.models.geometry.geom_components.wing.components.compute_mfw import ComputeMFW
from fastoad.models.geometry.geom_components.wing.components.compute_sweep_wing import (
ComputeSweepWing,
)
from fastoad.models.geometry.geom_components.wing.components.compute_toc_wing import ComputeToCWing
from fastoad.models.geometry.geom_components.wing.components.compute_wet_area_wing import (
ComputeWetAreaWing,
)
from fastoad.models.geometry.geom_components.wing.components.compute_x_wing import ComputeXWing
from fastoad.models.geometry.geom_components.wing.components.compute_y_wing import ComputeYWing
[docs]class ComputeWingGeometry(Group):
# TODO: Document equations. Cite sources
""" Wing geometry estimation """
[docs] def setup(self):
self.add_subsystem("y_wing", ComputeYWing(), promotes=["*"])
self.add_subsystem("l14_wing", ComputeL1AndL4Wing(), promotes=["*"])
self.add_subsystem("l2l3_wing", ComputeL2AndL3Wing(), promotes=["*"])
self.add_subsystem("x_wing", ComputeXWing(), promotes=["*"])
self.add_subsystem("mac_wing", ComputeMACWing(), promotes=["*"])
self.add_subsystem("b50_wing", ComputeB50(), promotes=["*"])
self.add_subsystem("sweep_wing", ComputeSweepWing(), promotes=["*"])
self.add_subsystem("toc_wing", ComputeToCWing(), promotes=["*"])
self.add_subsystem("wetarea_wing", ComputeWetAreaWing(), promotes=["*"])
self.add_subsystem("clapha_wing", ComputeCLalpha(), promotes=["*"])
self.add_subsystem("mfw", ComputeMFW(), promotes=["*"])