"""
Python module for vertical tail sweep angle calculations, part of the vertical tail geometry.
"""
# 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 .compute_vt_sweep_0 import ComputeVTSweep0
from .compute_vt_sweep_50 import ComputeVTSweep50
from .compute_vt_sweep_100 import ComputeVTSweep100
from ..constants import SERVICE_VT_SWEEP, SUBMODEL_VT_SWEEP_LEGACY
# pylint: disable=too-few-public-methods
[docs]@oad.RegisterSubmodel(SERVICE_VT_SWEEP, SUBMODEL_VT_SWEEP_LEGACY)
class ComputeVTSweep(om.Group):
# TODO: Document equations. Cite sources
"""Vertical tail sweeps estimation."""
# pylint: disable=missing-function-docstring
# Overriding OpenMDAO setup
[docs] def setup(self):
self.add_subsystem(
"VT_sweep_0",
ComputeVTSweep0(),
promotes=["*"],
)
self.add_subsystem(
"VT_sweep_50",
ComputeVTSweep50(),
promotes=["*"],
)
self.add_subsystem(
"VT_sweep_100",
ComputeVTSweep100(),
promotes=["*"],
)