"""Constants for aerodynamics models."""
# 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/>.
from aenum import Enum
POLAR_POINT_COUNT = 150
SERVICE_OSWALD_COEFFICIENT = "service.aerodynamics.oswald_coefficient"
SERVICE_INDUCED_DRAG_COEFFICIENT = "service.aerodynamics.induced_drag_coefficient"
SERVICE_REYNOLDS_COEFFICIENT = "service.aerodynamics.reynolds_coefficient"
SERVICE_INITIALIZE_CL = "service.aerodynamics.initialize_CL"
SERVICE_CD0 = "service.aerodynamics.CD0"
SERVICE_CD0_WING = "service.aerodynamics.CD0.wing"
SERVICE_CD0_FUSELAGE = "service.aerodynamics.CD0.fuselage"
SERVICE_CD0_HORIZONTAL_TAIL = "service.aerodynamics.CD0.horizontal_tail"
SERVICE_CD0_VERTICAL_TAIL = "service.aerodynamics.CD0.vertical_tail"
SERVICE_CD0_NACELLES_PYLONS = "service.aerodynamics.CD0.nacelles_pylons"
SERVICE_CD0_SUM = "service.aerodynamics.CD0.sum"
SERVICE_CD_COMPRESSIBILITY = "service.aerodynamics.CD.compressibility"
SERVICE_CD_TRIM = "service.aerodynamics.CD.trim"
SERVICE_POLAR = "service.aerodynamics.polar"
SERVICE_HIGH_LIFT = "service.aerodynamics.high_lift"
SERVICE_XFOIL = "service.aerodynamics.xfoil"
SERVICE_LANDING_MAX_CL_CLEAN = "service.aerodynamics.landing.max_CL_clean"
SERVICE_LANDING_MAX_CL = "service.aerodynamics.landing.max_CL"
SERVICE_LANDING_MACH_REYNOLDS = "service.aerodynamics.landing.mach_reynolds"
SERVICE_LOW_SPEED_CL_AOA = "service.aerodynamics.low_speed.CL_AoA"
[docs]class PolarType(Enum):
"""Enumeration of polar types to be computed."""
HIGH_SPEED = "high_speed"
LOW_SPEED = "low_speed"
TAKEOFF = "takeoff"
LANDING = "landing"