Source code for RCAIDE.Library.Methods.Aerodynamics.Athena_Vortex_Lattice.AVL_Objects.Configuration
# RCAIDE/Library/Methods/Aerodynamics/Athena_Vortex_Lattice/AVL_Objects/Configuration.py
#
# Created: Oct 2024, M. Clarke
# ----------------------------------------------------------------------------------------------------------------------
# IMPORT
# ----------------------------------------------------------------------------------------------------------------------
# RCAIDE imports
from RCAIDE.Framework.Core import Data
# ----------------------------------------------------------------------------------------------------------------------
# Inputs
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[docs]
class Configuration(Data):
"""A data class defining the reference parameters of the aircraft geometry and
flight configuration
Assumptions:
None
Source:
None
Inputs:
None
Outputs:
None
Properties Used:
N/A
"""
def __defaults__(self):
""" Defines the data structure and defaults for mass properties of the aircraft
in AVL
Assumptions:
None
Source:
None
Inputs:
None
Outputs:
None
Properties Used:
N/A
"""
self.tag = 'configuration'
self.parasite_drag = 0.0
self.reference_values = Data()
self.reference_values.sref = 0.0 # [m]
self.reference_values.bref = 0.0 # [m]
self.reference_values.cref = 0.0 # [m]
self.reference_values.cg_coords = [0.,0.,0.] # [m]
self.mass_properties = Data()
self.mass_properties.inertial = Data()
self.mass_properties.mass = 0.0 # [kg]
self.mass_properties.inertial.Ixx = 0.0 # [kg.m^2]
self.mass_properties.inertial.Iyy = 0.0 # [kg.m^2]
self.mass_properties.inertial.Izz = 0.0 # [kg.m^2]
self.mass_properties.inertial.Ixy = 0.0 # [kg.m^2]
self.mass_properties.inertial.Iyz = 0.0 # [kg.m^2]
self.mass_properties.inertial.Izx = 0.0 # [kg.m^2]
self.symmetry_settings = Data()
self.symmetry_settings.Iysym = 0 # Assumed y-symmetry of solution # (1: symmetric, -1: antisymmetric, 0: no symmetry assumed)
self.symmetry_settings.Izsym = 0 # Assumed z-symmetry of solution
self.symmetry_settings.Zsym = 0.0 # z-coordinate of plane of z-symmetry
