Index

A

ABORT (cdadt.artifacts.TakeoffTrajectory attribute) ABSCISSA (cdadt.artifacts.MissionTrajectory attribute) (cdadt.artifacts.TakeoffTrajectory attribute) active (cdadt.certification.ConstraintResult property) (cdadt.optimization.OptimizationOutcome property) ACTIVE_TOLERANCE (cdadt.certification.ConstraintResult attribute) add() (cdadt.disciplines.base.Discipline method) (cdadt.disciplines.performance.Performance method) (cdadt.disciplines.structures.Structures method) adder (cdadt.config.Scaling property) AeroCoefficients (class in cdadt.models.coefficients) AerodynamicLoads (class in cdadt.models.loads) AerodynamicLoadsComp (class in cdadt.adapter.loads) Aerodynamics (class in cdadt.disciplines.aerodynamics) aircraft (cdadt.analysis.SizingAnalysis property) Aircraft (class in cdadt.aircraft) aircraft() (cdadt.adapter.lattice.DifferentiableLattice static method) AIRCRAFT_VARIABLES (cdadt.adapter.analysis.SizingMissionAnalysis attribute) AircraftError ALLOWED (cdadt.config.BlackBoxConfig attribute) (cdadt.config.Config attribute) (cdadt.config.ConstraintSpec attribute) (cdadt.config.DriverConfig attribute) (cdadt.config.ObjectiveSpec attribute) (cdadt.config.OptimizeSpec attribute) (cdadt.config.Scaling attribute) (cdadt.config.SolverConfig attribute) (cdadt.config.VariableSpec attribute)

altitude (cdadt.models.loads.FlightCondition property) analysis (cdadt.optimization.Optimizer property) ANGLES_OF_ATTACK (in module cdadt.adapter.lattice) ANGLES_OF_ATTACK_DEG (in module cdadt.adapter.oas) apply() (cdadt.aircraft.Aircraft method) (cdadt.disciplines.base.Discipline method) (cdadt.disciplines.performance.Performance method) (cdadt.mission.InitialConditions method) archive() (cdadt.cli.StudyCommand method) area (cdadt.models.loads.Planform property) (cdadt.models.planform.TrapezoidalPlanform property) ArtifactError as_kwargs() (cdadt.config.Bounds method) (cdadt.config.ObjectiveSpec method) (cdadt.config.OptimizeSpec method) (cdadt.config.Scaling method) as_number() (cdadt.config.CaseFileSection static method) as_number_or_vector() (cdadt.config.CaseFileSection static method) aspect_ratio (cdadt.models.loads.Planform property) (cdadt.models.planform.TrapezoidalPlanform property) atol (cdadt.blackbox.SolverSettings property) available (cdadt.artifacts.MissionTrajectory property) (cdadt.artifacts.TakeoffTrajectory property)

B

baseline (cdadt.optimization.OptimizationOutcome property) basis (cdadt.optimization.Optimizer property) black_box (cdadt.config.Config property) BlackBoxConfig (class in cdadt.config) BlackBoxError bounds (cdadt.config.ConstraintSpec property) (cdadt.config.OptimizeSpec property) Bounds (class in cdadt.config)

box (cdadt.analysis.SizingAnalysis property) build() (cdadt.adapter.avl.OpenAVLLoads class method) (cdadt.adapter.oas.OpenAeroStructLoads class method) (cdadt.analysis.SizingAnalysis method) (cdadt.blackbox.OpenConceptSizingBox method) (cdadt.models.loads.AerodynamicLoads class method) (cdadt.models.polar.PolarLoads class method) by_discipline (cdadt.results.SizingResults property)

C

CaseFileSection (class in cdadt.config) catalog (cdadt.analysis.SizingAnalysis property) CD (cdadt.models.coefficients.AeroCoefficients property) cdadt.adapter module cdadt.adapter.aircraft module cdadt.adapter.analysis module cdadt.adapter.avl module cdadt.adapter.lattice module cdadt.adapter.loads module cdadt.adapter.oas module cdadt.adapter.sections module cdadt.aircraft module cdadt.analysis module cdadt.artifacts module cdadt.blackbox module cdadt.certification module cdadt.cli module cdadt.config module cdadt.disciplines.aerodynamics module cdadt.disciplines.base module cdadt.disciplines.geometry module cdadt.disciplines.performance module cdadt.disciplines.propulsion module cdadt.disciplines.stability module cdadt.disciplines.structures module cdadt.disciplines.weights module cdadt.mission module cdadt.models module cdadt.models.coefficients module cdadt.models.loads module cdadt.models.planform module cdadt.models.polar module cdadt.optimization module

cdadt.parameters module cdadt.results module CdadtAircraftModel (class in cdadt.adapter.aircraft) certification (cdadt.analysis.SizingAnalysis property) CertificationBasis (class in cdadt.certification) changes() (cdadt.optimization.OptimizationOutcome method) check() (cdadt.mission.InitialConditions method) check_addressable() (cdadt.blackbox.OpenConceptSizingBox method) check_settable() (cdadt.blackbox.OpenConceptSizingBox method) child_of() (cdadt.config.CaseFileSection method) chord (cdadt.models.planform.WingSection property) CL (cdadt.models.coefficients.AeroCoefficients property) Cl (cdadt.models.coefficients.AeroCoefficients property) CL (cdadt.models.loads.FlightCondition property) clear() (cdadt.adapter.lattice.LatticeLibrary method) Cm (cdadt.models.coefficients.AeroCoefficients property) Cn (cdadt.models.coefficients.AeroCoefficients property) COEFFICIENTS (cdadt.adapter.lattice.LatticePolar attribute) coefficients (cdadt.adapter.lattice.LatticePolar property) coefficients() (cdadt.adapter.avl.OpenAVLLoads method) (cdadt.adapter.oas.OpenAeroStructLoads method) (cdadt.models.loads.AerodynamicLoads method) (cdadt.models.polar.PolarLoads method) coefficients_at() (cdadt.adapter.oas.OpenAeroStructLattice method) collect() (cdadt.aircraft.Aircraft method) (cdadt.disciplines.base.Discipline method) (cdadt.results.SizingResults class method) Command (class in cdadt.cli) CommandLineInterface (class in cdadt.cli) commands (cdadt.cli.CommandLineInterface property) compute() (cdadt.adapter.loads.AerodynamicLoadsComp method) (cdadt.adapter.sections.WingSectionsComp method) compute_partials() (cdadt.adapter.loads.AerodynamicLoadsComp method) (cdadt.adapter.sections.WingSectionsComp method) conditions (cdadt.disciplines.performance.Performance property) (cdadt.mission.ContinuationStep property) config (cdadt.analysis.SizingAnalysis property) Config (class in cdadt.config) ConfigError configure() (cdadt.cli.Command method) (cdadt.cli.InspectCommand method) (cdadt.cli.StudyCommand method) constraint (cdadt.certification.ConstraintResult property) Constraint (class in cdadt.certification) ConstraintError ConstraintResult (class in cdadt.certification) constraints (cdadt.certification.CertificationBasis property) (cdadt.config.Config property) (cdadt.optimization.OptimizationOutcome property) ConstraintSpec (class in cdadt.config) continuation (cdadt.config.Config property) ContinuationLadder (class in cdadt.mission) ContinuationStep (class in cdadt.mission) CONTINUE (cdadt.artifacts.TakeoffTrajectory attribute) converge() (cdadt.analysis.SizingAnalysis method) (cdadt.disciplines.performance.Performance method) (cdadt.mission.ContinuationLadder method) curvature (cdadt.adapter.lattice.LatticePolar property) CY (cdadt.models.coefficients.AeroCoefficients property)

D

decision_speed (cdadt.artifacts.TakeoffTrajectory property) DEFAULT_COMMANDS (in module cdadt.cli) DEFAULT_ROOT (cdadt.blackbox.RunDirectory attribute) derivative_mode (cdadt.config.DriverConfig property) describe() (cdadt.blackbox.OpenConceptSizingBox class method) (cdadt.config.Bounds method) describes (cdadt.adapter.lattice.LatticePolar property) description (cdadt.disciplines.aerodynamics.Aerodynamics attribute) (cdadt.disciplines.base.Discipline attribute) (cdadt.disciplines.geometry.Geometry attribute) (cdadt.disciplines.performance.Performance attribute) (cdadt.disciplines.propulsion.Propulsion attribute) (cdadt.disciplines.stability.Stability attribute) (cdadt.disciplines.structures.Structures attribute) (cdadt.disciplines.weights.Weights attribute) (cdadt.mission.ContinuationStep property) (cdadt.parameters.Response property) design_variables (cdadt.config.Config property) (cdadt.optimization.Optimizer property) DifferentiableLattice (class in cdadt.adapter.lattice) direction (cdadt.config.ObjectiveSpec property) directory (cdadt.artifacts.StudyArtifacts property) Discipline (class in cdadt.disciplines.base)

discipline_name (cdadt.disciplines.aerodynamics.Aerodynamics attribute) (cdadt.disciplines.base.Discipline property) (cdadt.disciplines.geometry.Geometry attribute) (cdadt.disciplines.performance.Performance attribute) (cdadt.disciplines.propulsion.Propulsion attribute) (cdadt.disciplines.stability.Stability attribute) (cdadt.disciplines.structures.Structures attribute) (cdadt.disciplines.weights.Weights attribute) DisciplineError disciplines (cdadt.aircraft.Aircraft property) (cdadt.analysis.SizingAnalysis property) drag() (cdadt.models.loads.AerodynamicLoads method) drag_at() (cdadt.adapter.lattice.LatticePolar method) DRAG_DEPENDS_ON (cdadt.adapter.avl.OpenAVLLoads attribute) (cdadt.adapter.oas.OpenAeroStructLoads attribute) (cdadt.models.loads.AerodynamicLoads attribute) (cdadt.models.polar.PolarLoads attribute) drag_gradients() (cdadt.adapter.avl.OpenAVLLoads method) (cdadt.adapter.oas.OpenAeroStructLoads method) (cdadt.models.loads.AerodynamicLoads method) (cdadt.models.polar.PolarLoads method) driver (cdadt.config.Config property) DriverConfig (class in cdadt.config) dynamic_pressure (cdadt.models.loads.FlightCondition property)

E

entries() (cdadt.config.CaseFileSection method) equals (cdadt.config.Bounds property) err_on_non_converge (cdadt.blackbox.SolverSettings property) evaluate() (cdadt.certification.CertificationBasis method) (cdadt.certification.Constraint method)

execute() (cdadt.cli.Command method) (cdadt.cli.InspectCommand method) (cdadt.cli.OptimizeCommand method) (cdadt.cli.SizeCommand method)

F

far_field_at() (cdadt.adapter.lattice.DifferentiableLattice method) fit() (cdadt.adapter.lattice.DifferentiableLattice method) (cdadt.adapter.lattice.LatticeSolver method) (cdadt.adapter.oas.OpenAeroStructLattice method) FlightCondition (class in cdadt.models.loads) for_case() (cdadt.blackbox.RunDirectory class method) free_variables (cdadt.config.Config property) from_dict() (cdadt.config.Config class method) from_section() (cdadt.config.BlackBoxConfig class method) (cdadt.config.Config class method) (cdadt.config.ConstraintSpec class method) (cdadt.config.DriverConfig class method) (cdadt.config.ObjectiveSpec class method) (cdadt.config.OptimizeSpec class method) (cdadt.config.Scaling class method) (cdadt.config.SolverConfig class method) (cdadt.config.VariableSpec class method)

from_specs() (cdadt.certification.CertificationBasis class method) from_yaml() (cdadt.config.Config class method)

G

GEOMETRY (cdadt.adapter.lattice.LatticePolar attribute) Geometry (class in cdadt.disciplines.geometry) geometry() (cdadt.models.planform.TrapezoidalPlanform static method)

get() (cdadt.blackbox.OpenConceptSizingBox method) (cdadt.config.CaseFileSection method) gradient() (cdadt.adapter.lattice.LatticePolar method) GRADIENT_NAMES (cdadt.models.loads.AerodynamicLoads attribute)

H

HALVES (cdadt.cli.InspectCommand attribute) has() (cdadt.blackbox.OpenConceptSizingBox method) help (cdadt.cli.Command attribute) (cdadt.cli.InspectCommand attribute) (cdadt.cli.OptimizeCommand attribute) (cdadt.cli.SizeCommand attribute)

I

INDEP_VAR_TAG (cdadt.blackbox.OpenConceptSizingBox attribute) index (cdadt.config.ObjectiveSpec property) indices (cdadt.config.ConstraintSpec property) (cdadt.config.OptimizeSpec property) induced_drag_factor() (cdadt.models.polar.PolarLoads method) initial_conditions() (cdadt.config.Config method) initial_conditions_specs (cdadt.config.Config property) InitialConditions (class in cdadt.mission) initialize() (cdadt.adapter.aircraft.CdadtAircraftModel method) (cdadt.adapter.analysis.SizingMissionAnalysis method) (cdadt.adapter.loads.AerodynamicLoadsComp method) (cdadt.adapter.sections.WingSectionsComp method)

InspectCommand (class in cdadt.cli) iprint (cdadt.blackbox.SolverSettings property) is_built (cdadt.blackbox.OpenConceptSizingBox property) is_empty (cdadt.config.Scaling property) is_equality (cdadt.config.Bounds property) is_free (cdadt.config.VariableSpec property) is_optimization (cdadt.config.Config property) is_scalar (cdadt.blackbox.VariableInfo property) is_traceable (cdadt.certification.Constraint property) (cdadt.config.ConstraintSpec property) is_two_sided (cdadt.config.Bounds property)

J

jacobian (cdadt.adapter.lattice.LatticePolar property)

jet_transport_zero_lift_drag() (in module cdadt.adapter.analysis)

K

kind (cdadt.blackbox.VariableInfo property)

L

label (cdadt.artifacts.Trace property) ladder (cdadt.disciplines.performance.Performance property) lateral_directional (cdadt.models.coefficients.AeroCoefficients property) LatticeLibrary (class in cdadt.adapter.lattice) LatticePolar (class in cdadt.adapter.lattice)

LatticeSolver (class in cdadt.adapter.lattice) lift_at_minimum_drag (cdadt.adapter.lattice.LatticePolar property) linear (cdadt.config.ConstraintSpec property) LoadsError lower (cdadt.config.Bounds property) (cdadt.config.OptimizeSpec property)

M

mach (cdadt.models.loads.FlightCondition property) MACH_SAMPLES (in module cdadt.adapter.avl) magnitude (cdadt.config.Bounds property) main() (in module cdadt.cli) margin (cdadt.certification.ConstraintResult property) maxiter (cdadt.blackbox.SolverSettings property) (cdadt.config.DriverConfig property) (cdadt.config.SolverConfig property) mean_aerodynamic_chord (cdadt.models.planform.TrapezoidalPlanform property) merged_with() (cdadt.mission.InitialConditions method) MESH_INPUTS (cdadt.adapter.oas.OpenAeroStructLattice attribute) minimum_drag (cdadt.adapter.lattice.LatticePolar property) missing (cdadt.results.SizingResults property) missing() (cdadt.aircraft.Aircraft method) (cdadt.disciplines.base.Discipline method) mission_path (cdadt.config.Config property) (cdadt.mission.InitialConditions property) MissionError MissionTrajectory (class in cdadt.artifacts) model (cdadt.blackbox.OpenConceptSizingBox property) (cdadt.config.BlackBoxConfig property) (cdadt.results.SizingResults property) model_class (cdadt.blackbox.OpenConceptSizingBox property) model_name (cdadt.adapter.avl.OpenAVLLoads attribute) (cdadt.adapter.oas.OpenAeroStructLoads attribute) (cdadt.models.loads.AerodynamicLoads attribute) (cdadt.models.polar.PolarLoads attribute) model_options (cdadt.blackbox.OpenConceptSizingBox property) model_spec (cdadt.blackbox.OpenConceptSizingBox property) MODES (cdadt.config.DriverConfig attribute) module cdadt.adapter cdadt.adapter.aircraft cdadt.adapter.analysis cdadt.adapter.avl cdadt.adapter.lattice cdadt.adapter.loads cdadt.adapter.oas cdadt.adapter.sections cdadt.aircraft cdadt.analysis cdadt.artifacts cdadt.blackbox cdadt.certification cdadt.cli cdadt.config cdadt.disciplines.aerodynamics cdadt.disciplines.base cdadt.disciplines.geometry cdadt.disciplines.performance cdadt.disciplines.propulsion cdadt.disciplines.stability cdadt.disciplines.structures cdadt.disciplines.weights cdadt.mission cdadt.models cdadt.models.coefficients cdadt.models.loads cdadt.models.planform cdadt.models.polar cdadt.optimization cdadt.parameters cdadt.results

N

name (cdadt.artifacts.Trace property) (cdadt.blackbox.RunDirectory property) (cdadt.blackbox.VariableInfo property) (cdadt.certification.Constraint property) (cdadt.cli.Command attribute) (cdadt.cli.InspectCommand attribute) (cdadt.cli.OptimizeCommand attribute) (cdadt.cli.SizeCommand attribute) (cdadt.config.ConstraintSpec property) (cdadt.config.DriverConfig property) (cdadt.config.ObjectiveSpec property) (cdadt.config.VariableSpec property) (cdadt.parameters.Parameter property) (cdadt.parameters.Response property)

NAMES (cdadt.models.coefficients.AeroCoefficients attribute) (cdadt.models.loads.FlightCondition attribute) new_workspace() (cdadt.adapter.avl.OpenAVLLoads class method) (cdadt.adapter.oas.OpenAeroStructLoads class method) (cdadt.models.loads.AerodynamicLoads class method) num_nodes (cdadt.blackbox.OpenConceptSizingBox property) (cdadt.config.BlackBoxConfig property) (cdadt.results.SizingResults property) number_or_vector() (cdadt.config.CaseFileSection method)

O

objective (cdadt.config.Config property) (cdadt.optimization.OptimizationOutcome property) objective_path (cdadt.optimization.Optimizer property) objective_units (cdadt.optimization.Optimizer property) ObjectiveSpec (class in cdadt.config) openaerostruct_is_available() (in module cdadt.adapter.oas) OpenAeroStructLattice (class in cdadt.adapter.oas) OpenAeroStructLoads (class in cdadt.adapter.oas) openavl_is_available() (in module cdadt.adapter.avl) OpenAVLLoads (class in cdadt.adapter.avl) OpenConceptSizingBox (class in cdadt.blackbox) OptimizationError OptimizationOutcome (class in cdadt.optimization) optimize (cdadt.config.VariableSpec property) OptimizeCommand (class in cdadt.cli) Optimizer (class in cdadt.optimization)

OptimizeSpec (class in cdadt.config) optimum (cdadt.optimization.OptimizationOutcome property) optional (cdadt.parameters.Response property) options (cdadt.config.BlackBoxConfig property) (cdadt.config.DriverConfig property) owned_patterns (cdadt.disciplines.aerodynamics.Aerodynamics attribute) (cdadt.disciplines.base.Discipline attribute) (cdadt.disciplines.geometry.Geometry attribute) (cdadt.disciplines.performance.Performance attribute) (cdadt.disciplines.propulsion.Propulsion attribute) (cdadt.disciplines.stability.Stability attribute) (cdadt.disciplines.structures.Structures attribute) (cdadt.disciplines.weights.Weights attribute) owner() (cdadt.aircraft.Aircraft method) (cdadt.results.ResponseCatalog method) owns() (cdadt.disciplines.base.Discipline class method)

P

Parameter (class in cdadt.parameters) parameter() (cdadt.config.VariableSpec method) (cdadt.disciplines.base.Discipline method) parameters (cdadt.aircraft.Aircraft property) (cdadt.disciplines.base.Discipline property) parameters() (cdadt.config.Config method) parser() (cdadt.cli.CommandLineInterface method) path (cdadt.blackbox.RunDirectory property) (cdadt.certification.Constraint property) (cdadt.config.Config property) (cdadt.parameters.Response property) path() (cdadt.artifacts.TakeoffTrajectory method) (cdadt.artifacts.Trace method) (cdadt.results.ResponseCatalog method)

performance (cdadt.analysis.SizingAnalysis property) Performance (class in cdadt.disciplines.performance) PHASE_MARKER (cdadt.artifacts.MissionTrajectory attribute) phases (cdadt.artifacts.MissionTrajectory property) Planform (class in cdadt.models.loads) polar() (cdadt.adapter.oas.OpenAeroStructLoads method) polar_at() (cdadt.adapter.avl.OpenAVLLoads method) polar_for() (cdadt.adapter.lattice.LatticeLibrary method) PolarLoads (class in cdadt.models.polar) prepare() (cdadt.optimization.Optimizer method) problem (cdadt.blackbox.OpenConceptSizingBox property) problem() (cdadt.blackbox.RunDirectory method) PROFILE_PANELS (cdadt.artifacts.StudyArtifacts attribute) Propulsion (class in cdadt.disciplines.propulsion)

R

read() (cdadt.artifacts.MissionTrajectory method) readable() (cdadt.blackbox.OpenConceptSizingBox method) ref (cdadt.config.OptimizeSpec property) (cdadt.config.Scaling property) ref0 (cdadt.config.Scaling property) register() (cdadt.certification.CertificationBasis method) (cdadt.certification.Constraint method) regulation (cdadt.certification.Constraint property) (cdadt.config.ConstraintSpec property) reject_unknown() (cdadt.config.CaseFileSection method) relative_margin (cdadt.certification.ConstraintResult property) replace() (cdadt.parameters.Parameter method) report() (cdadt.optimization.Optimizer method) (cdadt.results.SizingResults method) reported (cdadt.disciplines.aerodynamics.Aerodynamics attribute) (cdadt.disciplines.base.Discipline attribute) (cdadt.disciplines.geometry.Geometry attribute) (cdadt.disciplines.performance.Performance attribute) (cdadt.disciplines.propulsion.Propulsion attribute) (cdadt.disciplines.stability.Stability attribute) (cdadt.disciplines.structures.Structures attribute) (cdadt.disciplines.weights.Weights attribute)

require() (cdadt.config.CaseFileSection method) resample() (cdadt.mission.InitialConditions method) resolve() (cdadt.mission.InitialConditions method) Response (class in cdadt.parameters) response() (cdadt.results.ResponseCatalog method) ResponseCatalog (class in cdadt.results) results() (cdadt.analysis.SizingAnalysis method) root (cdadt.blackbox.RunDirectory property) root_chord (cdadt.models.planform.TrapezoidalPlanform property) rtol (cdadt.blackbox.SolverSettings property) run() (cdadt.analysis.SizingAnalysis method) (cdadt.blackbox.OpenConceptSizingBox method) (cdadt.cli.CommandLineInterface method) (cdadt.mission.SupportsConditions method) (cdadt.optimization.Optimizer method) run_directory (cdadt.blackbox.OpenConceptSizingBox property) run_directory() (cdadt.cli.StudyCommand static method) run_driver() (cdadt.blackbox.OpenConceptSizingBox method) RunDirectory (class in cdadt.blackbox)

S

satisfied (cdadt.certification.ConstraintResult property) SCALAR_INPUTS (cdadt.adapter.loads.AerodynamicLoadsComp attribute) scalars() (cdadt.results.SizingResults method) scaler (cdadt.config.Scaling property) scaling (cdadt.config.ConstraintSpec property) (cdadt.config.ObjectiveSpec property) (cdadt.config.OptimizeSpec property) Scaling (class in cdadt.config) sections() (cdadt.models.planform.TrapezoidalPlanform method) sense (cdadt.config.ObjectiveSpec property) (cdadt.optimization.OptimizationOutcome property) SENSES (cdadt.config.ObjectiveSpec attribute) series() (cdadt.config.CaseFileSection method) set() (cdadt.aircraft.Aircraft method) (cdadt.blackbox.OpenConceptSizingBox method) (cdadt.disciplines.base.Discipline method) (cdadt.mission.SupportsConditions method) settable() (cdadt.blackbox.OpenConceptSizingBox method) settings() (cdadt.config.SolverConfig method) setup() (cdadt.adapter.aircraft.CdadtAircraftModel method) (cdadt.adapter.analysis.SizingMissionAnalysis method) (cdadt.adapter.loads.AerodynamicLoadsComp method) (cdadt.adapter.sections.WingSectionsComp method) shape (cdadt.blackbox.VariableInfo property) shape_of() (cdadt.blackbox.OpenConceptSizingBox method) (cdadt.mission.SupportsConditions method) SizeCommand (class in cdadt.cli)

SizingAnalysis (class in cdadt.analysis) SizingMissionAnalysis (class in cdadt.adapter.analysis) SizingResults (class in cdadt.results) solver (cdadt.adapter.lattice.LatticeLibrary property) (cdadt.blackbox.OpenConceptSizingBox property) (cdadt.config.Config property) SolverConfig (class in cdadt.config) SolverSettings (class in cdadt.blackbox) source (cdadt.certification.Constraint property) (cdadt.config.ConstraintSpec property) (cdadt.config.VariableSpec property) (cdadt.parameters.Parameter property) span (cdadt.models.planform.TrapezoidalPlanform property) span_efficiency (cdadt.adapter.avl.OpenAVLLoads property) (cdadt.adapter.lattice.LatticePolar property) (cdadt.adapter.oas.OpenAeroStructLoads property) (cdadt.models.polar.PolarLoads property) spec (cdadt.certification.Constraint property) Stability (class in cdadt.disciplines.stability) status (cdadt.certification.ConstraintResult property) steps (cdadt.mission.ContinuationLadder property) Structures (class in cdadt.disciplines.structures) StudyArtifacts (class in cdadt.artifacts) StudyCommand (class in cdadt.cli) succeeded (cdadt.optimization.OptimizationOutcome property) SupportsConditions (class in cdadt.mission) sweep (cdadt.models.planform.TrapezoidalPlanform property)

T

TAKEOFF_PHASES (cdadt.adapter.aircraft.CdadtAircraftModel attribute) TakeoffTrajectory (class in cdadt.artifacts) taper (cdadt.models.planform.TrapezoidalPlanform property) tip_chord (cdadt.models.planform.TrapezoidalPlanform property) title (cdadt.certification.Constraint property) (cdadt.config.ConstraintSpec property) to_dict() (cdadt.results.SizingResults method)

tol (cdadt.config.DriverConfig property) Trace (class in cdadt.artifacts) traceability_matrix() (cdadt.certification.CertificationBasis method) traceable (cdadt.certification.CertificationBasis property) TRACES (cdadt.artifacts.MissionTrajectory attribute) (cdadt.artifacts.TakeoffTrajectory attribute) TrapezoidalPlanform (class in cdadt.models.planform)

U

units (cdadt.artifacts.Trace property) (cdadt.blackbox.VariableInfo property) (cdadt.certification.Constraint property) (cdadt.config.ConstraintSpec property) (cdadt.config.ObjectiveSpec property) (cdadt.config.VariableSpec property) (cdadt.parameters.Parameter property) (cdadt.parameters.Response property)

units() (cdadt.disciplines.base.Discipline method) (cdadt.results.ResponseCatalog method) unowned() (cdadt.aircraft.Aircraft method) upper (cdadt.config.Bounds property) (cdadt.config.OptimizeSpec property)

V

V1_PATH (cdadt.artifacts.TakeoffTrajectory attribute) value (cdadt.certification.ConstraintResult property) (cdadt.config.VariableSpec property) (cdadt.parameters.Parameter property) value() (cdadt.aircraft.Aircraft method) (cdadt.disciplines.base.Discipline method)

values (cdadt.mission.InitialConditions property) VariableInfo (class in cdadt.blackbox) VariableSpec (class in cdadt.config) verbose_help (cdadt.cli.OptimizeCommand attribute) (cdadt.cli.StudyCommand attribute) violated (cdadt.optimization.OptimizationOutcome property)

W

Weights (class in cdadt.disciplines.weights) where (cdadt.config.CaseFileSection property) WingSection (class in cdadt.models.planform) WingSectionsComp (class in cdadt.adapter.sections) write_json() (cdadt.artifacts.StudyArtifacts method)

write_mission_profile() (cdadt.artifacts.StudyArtifacts method) write_n2() (cdadt.artifacts.StudyArtifacts method) write_takeoff() (cdadt.artifacts.StudyArtifacts method) write_text() (cdadt.artifacts.StudyArtifacts method) write_trajectory() (cdadt.artifacts.StudyArtifacts method) written() (cdadt.artifacts.StudyArtifacts method)

X

x (cdadt.models.planform.WingSection property)

Y

y (cdadt.models.planform.WingSection property)

Z

z (cdadt.models.planform.WingSection property)

zero_lift_drag (cdadt.models.polar.PolarLoads property)