Source code for fastoad.models.aerodynamics.components.compute_reynolds

"""
    FAST - Copyright (c) 2016 ONERA ISAE
"""

#  This file is part of FAST-OAD : A framework for rapid Overall Aircraft Design
#  Copyright (C) 2021 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 numpy as np
from openmdao.core.explicitcomponent import ExplicitComponent

from fastoad.model_base import AtmosphereSI


[docs]class ComputeReynolds(ExplicitComponent):
[docs] def initialize(self): self.options.declare("low_speed_aero", default=False, types=bool)
[docs] def setup(self): self.low_speed_aero = self.options["low_speed_aero"] if self.low_speed_aero: self.add_input("data:aerodynamics:aircraft:takeoff:mach", val=np.nan) self.add_output("data:aerodynamics:wing:low_speed:reynolds") else: self.add_input("data:TLAR:cruise_mach", val=np.nan) self.add_input("data:mission:sizing:main_route:cruise:altitude", val=np.nan, units="m") self.add_output("data:aerodynamics:wing:cruise:reynolds")
[docs] def setup_partials(self): self.declare_partials("*", "*", method="fd")
[docs] def compute(self, inputs, outputs): if self.low_speed_aero: mach = inputs["data:aerodynamics:aircraft:takeoff:mach"] altitude = 0.0 else: mach = inputs["data:TLAR:cruise_mach"] altitude = inputs["data:mission:sizing:main_route:cruise:altitude"] atm = AtmosphereSI(altitude) atm.mach = mach reynolds = atm.unitary_reynolds if self.low_speed_aero: outputs["data:aerodynamics:wing:low_speed:reynolds"] = reynolds else: outputs["data:aerodynamics:wing:cruise:reynolds"] = reynolds