"""
Python module for wing geometry calculation, part of the geometry component.
"""
# This file is part of FAST-OAD_CS23 : A framework for rapid Overall Aircraft Design
# Copyright (C) 2025 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/>.
import openmdao.api as om
import fastoad.api as oad
from .constants import (
SERVICE_WING_THICKNESS_RATIO,
SERVICE_WING_SPAN,
SERVICE_WING_HEIGHT,
SERVICE_WING_L1_L4,
SERVICE_WING_L2_L3,
SERVICE_WING_X_LOCAL,
SERVICE_WING_X_ABSOLUTE,
SERVICE_WING_B50,
SERVICE_WING_MAC,
SERVICE_WING_SWEEP,
SUBMODEL_WING_WET_AREA,
)
from ...constants import SERVICE_WING_GEOMETRY, SUBMODEL_WING_GEOMETRY_LEGACY
# pylint: disable=too-few-public-methods
[docs]@oad.RegisterSubmodel(SERVICE_WING_GEOMETRY, SUBMODEL_WING_GEOMETRY_LEGACY)
class ComputeWingGeometry(om.Group):
"""Wing geometry estimation, obtained from :cite:`supaero:2014`."""
# pylint: disable=missing-function-docstring
# Overriding OpenMDAO setup
[docs] def setup(self):
self.add_subsystem(
"wing_toc",
oad.RegisterSubmodel.get_submodel(SERVICE_WING_THICKNESS_RATIO),
promotes=["*"],
)
self.add_subsystem(
"wing_y", oad.RegisterSubmodel.get_submodel(SERVICE_WING_SPAN), promotes=["*"]
)
self.add_subsystem(
"wing_l1l4", oad.RegisterSubmodel.get_submodel(SERVICE_WING_L1_L4), promotes=["*"]
)
self.add_subsystem(
"wing_l2l3", oad.RegisterSubmodel.get_submodel(SERVICE_WING_L2_L3), promotes=["*"]
)
self.add_subsystem(
"wing_z", oad.RegisterSubmodel.get_submodel(SERVICE_WING_HEIGHT), promotes=["*"]
)
self.add_subsystem(
"wing_x", oad.RegisterSubmodel.get_submodel(SERVICE_WING_X_LOCAL), promotes=["*"]
)
self.add_subsystem(
"wing_MAC", oad.RegisterSubmodel.get_submodel(SERVICE_WING_MAC), promotes=["*"]
)
self.add_subsystem(
"wing_x_absolute",
oad.RegisterSubmodel.get_submodel(SERVICE_WING_X_ABSOLUTE),
promotes=["*"],
)
self.add_subsystem(
"wing_sweep", oad.RegisterSubmodel.get_submodel(SERVICE_WING_SWEEP), promotes=["*"]
)
self.add_subsystem(
"wing_b50", oad.RegisterSubmodel.get_submodel(SERVICE_WING_B50), promotes=["*"]
)
self.add_subsystem(
"wing_wet_area",
oad.RegisterSubmodel.get_submodel(SUBMODEL_WING_WET_AREA),
promotes=["*"],
)