Index

_

__getattr__() (component.VectorizedAttributes method) (component.VectorizedComponent method) (mesh.mesh.VectorizedDiscretization method) __getitem__() (caddee.ConditionsDict method) (component.ComponentDict method) (mesh.mesh.DiscretizationsDict method) (mesh.mesh.MeshContainer method) (mesh.meshers.CamberSurfaceDict method) (mesh.meshers.OneDBoxBeamDict method) (mesh.meshers.RotorDiscretizationDict method) __post_init__() (mesh.mesh.Discretization method) __setattr__() (component.VectorizedAttributes method) __setitem__() (component.ComponentDict method) (mesh.mesh.DiscretizationsDict method) (mesh.meshers.CamberSurfaceDict method) _add_geometry() (aircraft.components.wing.Wing method) _aft_points_parametric (mesh.meshers.OneDBoxBeam attribute) _airfoil_lower_para (mesh.meshers.CamberSurface attribute) _airfoil_upper_para (mesh.meshers.CamberSurface attribute) _bottom_grid_parametric (mesh.meshers.OneDBoxBeam attribute) _check_shape_consistency() (aircraft.conditions.aircraft_condition.AircraftCondition method) _chordwise_spacing (mesh.meshers.CamberSurface attribute) _compute_surface_area() (component.Component method) _constant_b_spline_1_dof_space (component.Component attribute) _cubic_b_spline_5_dof_space (component.Component attribute) _disk_parametric (mesh.meshers.RotorDiscretization attribute) _expand_variables() (aircraft.conditions.aircraft_condition.AircraftCondition method) _extract_geometric_quantities_from_ffd_block() (aircraft.components.fuselage.Fuselage method) (aircraft.components.rotor.Rotor method) (aircraft.components.wing.Wing method) (component.Component method) _find_system_component() (component.Component method) _fit_surface() (aircraft.components.wing.Wing method) _fore_points_parametric (mesh.meshers.OneDBoxBeam attribute) _front_grid_parametric (mesh.meshers.OneDBoxBeam attribute) _front_spar_geom (mesh.meshers.OneDBoxBeam attribute) _geom (mesh.meshers.CamberSurface attribute) (mesh.meshers.OneDBoxBeam attribute) (mesh.meshers.RotorDiscretization attribute) _half_wing (mesh.meshers.OneDBoxBeam attribute) _has_been_expanded (mesh.mesh.Discretization attribute) _instance_count (component.Component attribute) _is_broadcastable() (aircraft.conditions.aircraft_condition.AircraftCondition method) _is_copy (component.Component attribute) _is_vector() (aircraft.conditions.aircraft_condition.AircraftCondition method)

_LE_points_para (mesh.meshers.CamberSurface attribute) _LE_points_parametric (mesh.meshers.OneDBoxBeam attribute) _linear_b_spline_2_dof_space (component.Component attribute) _linear_b_spline_3_dof_space (component.Component attribute) _lower_wireframe_para (mesh.meshers.CamberSurface attribute) _make_ffd_block() (aircraft.components.wing.Wing method) (component.Component method) _material_properties (mesh.meshers.OneDBoxBeam attribute) _node_bottom_parametric (mesh.meshers.OneDBoxBeam attribute) _node_top_parametric (mesh.meshers.OneDBoxBeam attribute) _norm_beam_width (mesh.meshers.OneDBoxBeam attribute) _norm_node_center (mesh.meshers.OneDBoxBeam attribute) _num_chord_wise (mesh.meshers.CamberSurface attribute) _num_spanwise (mesh.meshers.CamberSurface attribute) _p1 (mesh.meshers.RotorDiscretization attribute) _p2 (mesh.meshers.RotorDiscretization attribute) _p3 (mesh.meshers.RotorDiscretization attribute) _p4 (mesh.meshers.RotorDiscretization attribute) _quadratic_b_spline_3_dof_space (component.Component attribute) _rear_grid_parametric (mesh.meshers.OneDBoxBeam attribute) _rear_spar_geom (mesh.meshers.OneDBoxBeam attribute) _setup_condition() (aircraft.conditions.aircraft_condition.ClimbCondition method) (aircraft.conditions.aircraft_condition.CruiseCondition method) (aircraft.conditions.aircraft_condition.HoverCondition method) _setup_ffd_block() (aircraft.components.fuselage.Fuselage method) (aircraft.components.rotor.Rotor method) (aircraft.components.wing.Wing method) (component.Component method) _setup_ffd_parameterization() (aircraft.components.fuselage.Fuselage method) (aircraft.components.rotor.Rotor method) (aircraft.components.wing.Wing method) (component.Component method) _setup_geometry() (aircraft.components.fuselage.Fuselage method) (aircraft.components.rotor.Rotor method) (aircraft.components.wing.Wing method) (component.Component method) _skip_ffd (component.Component attribute) _spar_geom (mesh.meshers.OneDBoxBeam attribute) _TE_points_para (mesh.meshers.CamberSurface attribute) _TE_points_parametric (mesh.meshers.OneDBoxBeam attribute) _top_grid_parametric (mesh.meshers.OneDBoxBeam attribute) _update() (mesh.meshers.CamberSurface method) (mesh.meshers.OneDBoxBeam method) (mesh.meshers.RotorDiscretization method) (mesh.meshers.ShellDiscretization method) _upper_wireframe_para (mesh.meshers.CamberSurface attribute)

A

ac_states (aircraft.conditions.aircraft_condition.ACQuantities attribute) (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) accel_norm (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.LinAngAccel attribute) ACQuantities (class in aircraft.conditions.aircraft_condition) actuate() (aircraft.components.rotor.Rotor method) (aircraft.components.wing.Wing method) (component.Component method) aircraft module Aircraft (class in aircraft.components.aircraft) aircraft.components module aircraft.components.aircraft module aircraft.components.fuselage module aircraft.components.powertrain module aircraft.components.rotor module aircraft.components.wing module aircraft.conditions module aircraft.conditions.aircraft_condition module aircraft.models module aircraft.models.aerodynamics module aircraft.models.aerodynamics.drag_buildup module aircraft.models.aerodynamics.simple_lift_model module

aircraft.models.atmosphere module aircraft.models.atmosphere.simple_atmosphere_model module aircraft.models.equations_of_motion module aircraft.models.equations_of_motion.six_dof_euler_flat_earth module aircraft.models.weights module aircraft.models.weights.general_aviation module aircraft.models.weights.general_aviation.general_aviation_weights module aircraft.models.weights.nasa_lpc module aircraft.models.weights.nasa_lpc.m4_nasa_lpc module aircraft.models.weights.weights_solver module AircraftCondition (class in aircraft.conditions.aircraft_condition) alpha_ML_mid_panel (mesh.meshers.CamberSurface attribute) altitude (aircraft.conditions.aircraft_condition.CruiseParameters attribute) (aircraft.conditions.aircraft_condition.HoverParameters attribute) AR (aircraft.components.wing.WingParameters attribute) (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) assemble_forces_and_moments() (aircraft.conditions.aircraft_condition.AircraftCondition method) (condition.Condition method) assemble_meshes() (configuration.Configuration method) assemble_system_mass_properties() (configuration.Configuration method) (configuration.VectorizedConfig method) atmos_state (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) atmos_states (aircraft.conditions.aircraft_condition.ACQuantities attribute)

B

base_configuration (caddee.CADDEE property) battery module

beam_height (mesh.meshers.OneDBoxBeam attribute) beam_width (mesh.meshers.OneDBoxBeam attribute) BeamMesh (class in mesh.meshers) bottom_skin_thickness (mesh.meshers.OneDBoxBeam attribute)

C

caddee module CADDEE (class in caddee) CamberSurface (class in mesh.meshers) CamberSurfaceDict (class in mesh.meshers) center_chord (aircraft.components.wing.WingGeometricQuantities attribute) chord_profile (mesh.meshers.RotorDiscretization attribute) Cl_0 (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) Cl_alpha (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) climb_gradient (aircraft.conditions.aircraft_condition.ClimbParameters attribute) ClimbCondition (class in aircraft.conditions.aircraft_condition) ClimbParameters (class in aircraft.conditions.aircraft_condition) component module Component (class in component) ComponentDict (class in component) ComponentParameters (class in component) ComponentQuantities (class in component) compute() (aircraft.conditions.aircraft_condition.EigenValueOperation method) compute_derivatives() (aircraft.conditions.aircraft_condition.EigenValueOperation method) compute_drag_build_up() (in module aircraft.models.aerodynamics.drag_buildup)

condition module Condition (class in condition) conditions (caddee.CADDEE property) ConditionsDict (class in caddee) configuration module Configuration (class in configuration) configuration (condition.Condition property) connect_component_geometries() (configuration.Configuration method) connectivity (mesh.meshers.ShellDiscretization attribute) construct_ribs_and_spars() (aircraft.components.wing.Wing method) convert_shape_to_action_string() (in module aircraft.conditions.aircraft_condition) copy() (configuration.Configuration method) (mesh.mesh.Discretization method) (mesh.mesh.SolverMesh method) (mesh.meshers.CamberSurface method) cosine_spacing() (in module mesh.meshers) create_subgeometry() (component.Component method) CruiseCondition (class in aircraft.conditions.aircraft_condition) CruiseParameters (class in aircraft.conditions.aircraft_condition)

D

d_fuse (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) dihedral (aircraft.components.wing.WingParameters attribute) dihedral_angle_left (aircraft.components.wing.WingGeometricQuantities attribute) dihedral_angle_right (aircraft.components.wing.WingGeometricQuantities attribute) Discretization (class in mesh.mesh) discretizations (mesh.mesh.SolverMesh attribute) (mesh.meshers.BeamMesh attribute) (mesh.meshers.RotorMeshes attribute) (mesh.meshers.VLMMesh attribute)

DiscretizationsDict (class in mesh.mesh) disk_mesh (mesh.meshers.RotorDiscretization attribute) dp_dt (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.LinAngAccel attribute) dq_dt (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.LinAngAccel attribute) dr_dt (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.LinAngAccel attribute) drag_parameters (component.ComponentQuantities property) du_dt (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.LinAngAccel attribute) dv_dt (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.LinAngAccel attribute) dw_dt (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.LinAngAccel attribute)

E

EigenValueOperation (class in aircraft.conditions.aircraft_condition) embedded_airfoil_model_alpha_stall (mesh.meshers.CamberSurface attribute) embedded_airfoil_model_Cd (mesh.meshers.CamberSurface attribute) embedded_airfoil_model_Cl (mesh.meshers.CamberSurface attribute) embedded_airfoil_model_Cp (mesh.meshers.CamberSurface attribute) evaluate() (aircraft.conditions.aircraft_condition.EigenValueOperation method) (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModel method) (aircraft.models.atmosphere.simple_atmosphere_model.SimpleAtmosphereModel method) (aircraft.models.equations_of_motion.six_dof_euler_flat_earth.SixDofEulerFlatEarthModel method) (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightModel method) (aircraft.models.weights.weights_solver.WeightsSolverModel method)

evaluate_avionics_weight() (aircraft.models.weights.general_aviation.general_aviation_weights.GeneralAviationWeights method) evaluate_fuselage_weight() (aircraft.models.weights.general_aviation.general_aviation_weights.GeneralAviationWeights method) evaluate_horizontal_tail_weight() (aircraft.models.weights.general_aviation.general_aviation_weights.GeneralAviationWeights method) evaluate_main_landing_gear_weight() (aircraft.models.weights.general_aviation.general_aviation_weights.GeneralAviationWeights method) evaluate_vertical_tail_weight() (aircraft.models.weights.general_aviation.general_aviation_weights.GeneralAviationWeights method) evaluate_wing_weight() (aircraft.models.weights.general_aviation.general_aviation_weights.GeneralAviationWeights method)

F

final_altitude (aircraft.conditions.aircraft_condition.ClimbParameters attribute) finalize_meshes() (aircraft.conditions.aircraft_condition.AircraftCondition method) (condition.Condition method)

flight_path_angle (aircraft.conditions.aircraft_condition.ClimbParameters attribute) Fuselage (class in aircraft.components.fuselage) FuselageGeometricQuantities (class in aircraft.components.fuselage) FuselageParameters (class in aircraft.components.fuselage)

G

GAInstrumentsWeightInputs (class in aircraft.models.weights.general_aviation.general_aviation_weights) GAInstrumentsWeightModel (class in aircraft.models.weights.general_aviation.general_aviation_weights)

GeneralAviationWeights (class in aircraft.models.weights.general_aviation.general_aviation_weights) geometry (mesh.meshers.ShellDiscretization attribute)

H

height (aircraft.components.fuselage.FuselageGeometricQuantities attribute) HoverCondition (class in aircraft.conditions.aircraft_condition)

HoverParameters (class in aircraft.conditions.aircraft_condition) hub_radius (aircraft.components.rotor.RotorParameters attribute)

I

import_shell_mesh() (in module mesh.meshers) incidence (aircraft.components.wing.WingParameters attribute) inertial_forces (aircraft.conditions.aircraft_condition.ACQuantities attribute)

inertial_moments (aircraft.conditions.aircraft_condition.ACQuantities attribute) initial_altitude (aircraft.conditions.aircraft_condition.ClimbParameters attribute) inverter module

L

LE_center (aircraft.components.wing.Wing property) LE_left_tip (aircraft.components.wing.Wing property) LE_right_tip (aircraft.components.wing.Wing property)

left_tip_chord (aircraft.components.wing.WingGeometricQuantities attribute) length (aircraft.components.fuselage.FuselageGeometricQuantities attribute) (aircraft.components.fuselage.FuselageParameters attribute) LinAngAccel (class in aircraft.models.equations_of_motion.six_dof_euler_flat_earth)

M

MAC (aircraft.components.wing.WingParameters attribute) mach_max (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightInputs attribute) mach_number (aircraft.conditions.aircraft_condition.ClimbParameters attribute) (aircraft.conditions.aircraft_condition.CruiseParameters attribute) make_1d_box_beam() (in module mesh.meshers) make_mesh_symmetric() (in module mesh.meshers) make_rotor_mesh() (in module mesh.meshers) make_vlm_surface() (in module mesh.meshers) mass_properties (component.ComponentQuantities property) material_properties (component.ComponentQuantities property) max_height (aircraft.components.fuselage.FuselageParameters attribute) max_sweep (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) max_width (aircraft.components.fuselage.FuselageParameters attribute) mesh module mesh.mesh module mesh.meshers module mesh_quality (mesh.mesh.Discretization attribute) MeshContainer (class in mesh.mesh) mid_panel_chord_length (mesh.meshers.CamberSurface attribute) module aircraft aircraft.components aircraft.components.aircraft aircraft.components.fuselage aircraft.components.powertrain aircraft.components.rotor aircraft.components.wing aircraft.conditions aircraft.conditions.aircraft_condition aircraft.models aircraft.models.aerodynamics aircraft.models.aerodynamics.drag_buildup aircraft.models.aerodynamics.simple_lift_model aircraft.models.atmosphere aircraft.models.atmosphere.simple_atmosphere_model aircraft.models.equations_of_motion aircraft.models.equations_of_motion.six_dof_euler_flat_earth aircraft.models.weights aircraft.models.weights.general_aviation aircraft.models.weights.general_aviation.general_aviation_weights aircraft.models.weights.nasa_lpc aircraft.models.weights.nasa_lpc.m4_nasa_lpc aircraft.models.weights.weights_solver battery caddee component condition configuration inverter mesh mesh.mesh mesh.meshers powertrain

N

nodal_coordinates (mesh.mesh.Discretization attribute) nodal_velocities (mesh.mesh.Discretization attribute) nodes_parametric (mesh.meshers.ShellDiscretization attribute) norm_hub_radius (mesh.meshers.RotorDiscretization attribute) num_azimuthal (mesh.meshers.RotorDiscretization attribute)

num_beam_nodes (mesh.meshers.OneDBoxBeam attribute) num_blades (mesh.meshers.RotorDiscretization attribute) num_flight_crew (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightInputs attribute) num_fuselage_mounted_engines (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightInputs attribute) num_radial (mesh.meshers.RotorDiscretization attribute) num_wing_mounted_engines (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightInputs attribute)

O

OneDBoxBeam (class in mesh.meshers)

OneDBoxBeamDict (class in mesh.meshers)

P

parent (component.Component attribute) perform_linear_stability_analysis() (aircraft.conditions.aircraft_condition.AircraftCondition method) pitch_angle (aircraft.conditions.aircraft_condition.ClimbParameters attribute) (aircraft.conditions.aircraft_condition.CruiseParameters attribute)

plot() (component.Component method) powertrain module Powertrain (class in aircraft.components.powertrain) project_airfoil_points() (mesh.meshers.CamberSurface method)

Q

quarter_chord (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute)

R

radius (aircraft.components.rotor.RotorParameters attribute) (mesh.meshers.RotorDiscretization attribute) range (aircraft.conditions.aircraft_condition.CruiseParameters attribute) rate_of_climb (aircraft.conditions.aircraft_condition.ClimbParameters attribute) recorder (in module aircraft.conditions.aircraft_condition) (in module aircraft.models.equations_of_motion.six_dof_euler_flat_earth) remove_component() (configuration.Configuration method)

reynolds_number (mesh.meshers.CamberSurface attribute) right_tip_chord (aircraft.components.wing.WingGeometricQuantities attribute) root_twist_delta (aircraft.components.wing.WingParameters attribute) Rotor (class in aircraft.components.rotor) RotorDiscretization (class in mesh.meshers) RotorDiscretizationDict (class in mesh.meshers) RotorMeshes (class in mesh.meshers) RotorParameters (class in aircraft.components.rotor)

S

S_fuse_planform (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightInputs attribute) S_ref (aircraft.components.wing.WingParameters attribute) (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) S_wet (aircraft.components.fuselage.FuselageParameters attribute) (aircraft.components.wing.WingParameters attribute) (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) setup_geometry() (configuration.Configuration method) shear_web_thickness (mesh.meshers.OneDBoxBeam attribute) ShellDiscretization (class in mesh.meshers) ShellMesh (class in mesh.meshers) SimpleAtmosphereModel (class in aircraft.models.atmosphere.simple_atmosphere_model)

SimpleLiftModel (class in aircraft.models.aerodynamics.simple_lift_model) SimpleLiftModelInputs (class in aircraft.models.aerodynamics.simple_lift_model) SixDofEulerFlatEarthModel (class in aircraft.models.equations_of_motion.six_dof_euler_flat_earth) SolverMesh (class in mesh.mesh) span (aircraft.components.wing.WingGeometricQuantities attribute) (aircraft.components.wing.WingParameters attribute) speed (aircraft.conditions.aircraft_condition.ClimbParameters attribute) (aircraft.conditions.aircraft_condition.CruiseParameters attribute) sweep (aircraft.components.wing.WingParameters attribute) sweep_angle_left (aircraft.components.wing.WingGeometricQuantities attribute) sweep_angle_right (aircraft.components.wing.WingGeometricQuantities attribute)

T

taper_ratio (aircraft.components.wing.WingParameters attribute) TE_center (aircraft.components.wing.Wing property) TE_left_tip (aircraft.components.wing.Wing property) TE_right_tip (aircraft.components.wing.Wing property) theta (in module aircraft.models.aerodynamics.simple_lift_model) thickness_to_chord (aircraft.components.wing.WingParameters attribute) thickness_to_chord_loc (aircraft.components.wing.WingParameters attribute)

thrust_origin (mesh.meshers.RotorDiscretization attribute) thrust_vector (mesh.meshers.RotorDiscretization attribute) time (aircraft.conditions.aircraft_condition.ClimbParameters attribute) (aircraft.conditions.aircraft_condition.CruiseParameters attribute) (aircraft.conditions.aircraft_condition.HoverParameters attribute) tip_twist_delta (aircraft.components.wing.WingParameters attribute) top_skin_thickness (mesh.meshers.OneDBoxBeam attribute) twist_profile (mesh.meshers.RotorDiscretization attribute)

U

unpack_attributes() (in module component) update() (aircraft.conditions.aircraft_condition.AircraftCondition method) (aircraft.conditions.aircraft_condition.ClimbCondition method) (aircraft.conditions.aircraft_condition.CruiseCondition method) (aircraft.conditions.aircraft_condition.HoverCondition method)

V

vectorized_configuration (condition.Condition property) vectorized_copy() (configuration.Configuration method) VectorizedAttributes (class in component) VectorizedComponent (class in component)

VectorizedConfig (class in configuration) VectorizedDiscretization (class in mesh.mesh) visualize_component_hierarchy() (configuration.Configuration method) VLMMesh (class in mesh.meshers)

W

W_wing_est (in module aircraft.models.weights.general_aviation.general_aviation_weights) WeightsSolverModel (class in aircraft.models.weights.weights_solver) width (aircraft.components.fuselage.FuselageGeometricQuantities attribute)

Wing (class in aircraft.components.wing) wing_incidence (aircraft.models.aerodynamics.simple_lift_model.SimpleLiftModelInputs attribute) WingGeometricQuantities (class in aircraft.components.wing) WingParameters (class in aircraft.components.wing)

X

xl (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightInputs attribute)

xlw (aircraft.models.weights.general_aviation.general_aviation_weights.GAInstrumentsWeightInputs attribute)