"""
FAST - Copyright (c) 2016 ONERA ISAE
"""
# 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.aerodynamics.aerodynamics_high_speed import AerodynamicsHighSpeed
from fastoad.models.aerodynamics.aerodynamics_landing import AerodynamicsLanding
from fastoad.models.aerodynamics.aerodynamics_low_speed import AerodynamicsLowSpeed
[docs]class Aerodynamics(Group):
[docs] def setup(self):
# Compute the low speed aero (Cl alpha at takeoff and Cl0)
self.add_subsystem("aero_low", AerodynamicsLowSpeed(), promotes=["*"])
# Compute CL max landing
self.add_subsystem("aero_landing", AerodynamicsLanding(), promotes=["*"])
# Compute cruise characteristics
self.add_subsystem("aero_high", AerodynamicsHighSpeed(), promotes=["*"])