Source code for fastga.models.load_analysis.wing.loads

#  This file is part of FAST-OAD_CS23 : A framework for rapid Overall Aircraft Design
#  Copyright (C) 2022  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.
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import openmdao.api as om

import fastoad.api as oad
from fastoad.module_management.constants import ModelDomain

from .constants import (
    SUBMODEL_AEROSTRUCTURAL_LOADS,
    SUBMODEL_STRUCTURAL_LOADS,
    SUBMODEL_AERODYNAMIC_LOADS,
)


[docs]@oad.RegisterOpenMDAOSystem("fastga.loads.wing", domain=ModelDomain.OTHER) class WingLoads(om.Group):
[docs] def setup(self): self.add_subsystem( "aerostructural_loads", oad.RegisterSubmodel.get_submodel(SUBMODEL_AEROSTRUCTURAL_LOADS), promotes=["*"], ) self.add_subsystem( "structural_loads", oad.RegisterSubmodel.get_submodel(SUBMODEL_STRUCTURAL_LOADS), promotes=["*"], ) self.add_subsystem( "aerodynamic_loads", oad.RegisterSubmodel.get_submodel(SUBMODEL_AERODYNAMIC_LOADS), promotes=["*"], )