Index A | B | C | D | E | F | G | H | I | J | K | L | M | N | O | P | R | S | T | U | V | W | X | Y | Z A A4_star (flight_mech.turbine.TurbojetSingleBody attribute) A8 (flight_mech.turbine.TurbojetSingleBody property) A8_star (flight_mech.turbine.TurbojetSingleBody property) Airfoil (class in flight_mech.airfoil) alpha_0 (flight_mech.plane.Plane attribute) alpha_f_max (flight_mech.plane.Plane property) alpha_stall (flight_mech.plane.Plane attribute) AMMONIAC (flight_mech.fuel.FuelTable attribute) aspect_ratio (flight_mech.wing.Wing property) atmosphere_model (flight_mech.plane.Plane attribute) AtmosphereModel (class in flight_mech.atmosphere) B b (flight_mech.plane.Plane attribute) base_airfoil (flight_mech.wing.Wing attribute) C C_D() (flight_mech.plane.Plane method) C_D_0 (flight_mech.plane.Plane attribute) C_L() (flight_mech.plane.Plane method) C_L_alpha (flight_mech.plane.Plane attribute) C_L_delta (flight_mech.plane.Plane attribute) C_L_f_max (flight_mech.plane.Plane property) C_L_max (flight_mech.plane.Plane attribute) C_m_0 (flight_mech.plane.Plane attribute) C_m_alpha (flight_mech.plane.Plane attribute) C_m_delta (flight_mech.plane.Plane attribute) camber_z_array (flight_mech.airfoil.Airfoil property) center_x_array (flight_mech.wing.Wing property) check_initialization() (flight_mech.wing.Wing method) check_pyvista_import() (in module flight_mech.wing) check_turbulent_transition() (in module flight_mech.aerodynamics) chord_length (flight_mech.airfoil.Airfoil property) chord_length_array (flight_mech.wing.Wing attribute) chord_z_array (flight_mech.airfoil.Airfoil property) compressor_efficiency (flight_mech.turbine.TurbojetSingleBody attribute) compute_airfoil_fourrier_coefficients() (flight_mech.airfoil.Airfoil method) compute_alpha_and_delta_at_flight_point() (flight_mech.plane.Plane method) compute_alpha_zero_lift() (flight_mech.airfoil.Airfoil method) compute_altitude_from_sigma() (flight_mech.atmosphere.AtmosphereModel static method) (flight_mech.atmosphere.ConstantAtmosphere static method) (flight_mech.atmosphere.LinearAtmosphere static method) (flight_mech.atmosphere.StandardAtmosphere class method) compute_ascension_slope() (flight_mech.plane.Plane method) compute_blasius_linear_drag() (in module flight_mech.aerodynamics) compute_blasius_rectangle_drag() (in module flight_mech.aerodynamics) compute_chord_min_and_max_for_trapezoidal_wing() (in module flight_mech.wing) compute_density_from_altitude() (flight_mech.atmosphere.AtmosphereModel class method) (flight_mech.atmosphere.ConstantAtmosphere class method) (flight_mech.atmosphere.LinearAtmosphere class method) (flight_mech.atmosphere.StandardAtmosphere class method) compute_drag() (flight_mech.plane.Plane method) compute_drag_with_ground_effect() (flight_mech.plane.Plane method) compute_dynamic_viscosity_from_altitude() (flight_mech.atmosphere.StandardAtmosphere class method) compute_endurance() (flight_mech.plane.Plane method) compute_fourrier_coefficients() (flight_mech.wing.Wing method) compute_gliding_speed() (flight_mech.plane.Plane method) compute_gliding_v_z_min() (flight_mech.plane.Plane method) compute_ground_effect() (flight_mech.plane.Plane method) compute_I_at_max_efficiency() (flight_mech.motor.ElectricalMotor method) compute_kinematic_viscosity_from_altitude() (flight_mech.atmosphere.StandardAtmosphere class method) compute_landing_distance() (flight_mech.plane.Plane method) compute_landing_speed() (flight_mech.plane.Plane method) compute_lift() (flight_mech.plane.Plane method) compute_lift_and_induced_drag_coefficients() (flight_mech.wing.Wing method) compute_lift_coefficient() (flight_mech.airfoil.Airfoil method) compute_linear_drag() (in module flight_mech.aerodynamics) compute_load_factor_from_roll_angle() (flight_mech.plane.Plane method) compute_max_altitude() (flight_mech.plane.Plane method) compute_max_ascension_slope() (flight_mech.plane.Plane method) compute_max_ascension_speed() (flight_mech.plane.Plane method) compute_max_gliding_range() (flight_mech.plane.Plane method) compute_max_gliding_time() (flight_mech.plane.Plane method) compute_max_range_at_fixed_altitude() (flight_mech.plane.Plane method) compute_min_descent_gliding_slope() (flight_mech.plane.Plane method) compute_min_thrust_needed() (flight_mech.plane.Plane method) compute_momentum_coefficient_at_aero_center() (flight_mech.airfoil.Airfoil method) compute_momentum_coefficient_at_leading_edge() (flight_mech.airfoil.Airfoil method) compute_normalized_thrust() (flight_mech.plane.Plane method) compute_polhausen_linear_drag() (in module flight_mech.aerodynamics) compute_pressure_from_altitude() (flight_mech.atmosphere.StandardAtmosphere static method) compute_range_at_fixed_speed() (flight_mech.plane.Plane method) compute_reference_speed() (flight_mech.plane.Plane method) compute_sigma_from_altitude() (flight_mech.atmosphere.AtmosphereModel static method) (flight_mech.atmosphere.ConstantAtmosphere static method) (flight_mech.atmosphere.LinearAtmosphere static method) (flight_mech.atmosphere.StandardAtmosphere class method) compute_simulation_linear_drag() (in module flight_mech.aerodynamics) compute_sound_speed_from_altitude() (flight_mech.atmosphere.StandardAtmosphere class method) compute_speed_for_max_ascension_speed() (flight_mech.plane.Plane method) compute_speed_for_min_power_needed() (flight_mech.plane.Plane method) compute_speed_for_min_thrust_needed() (flight_mech.plane.Plane method) compute_stall_speed() (flight_mech.plane.Plane method) compute_take_off_distance_no_friction() (flight_mech.plane.Plane method) compute_take_off_distance_with_friction() (flight_mech.plane.Plane method) compute_take_off_speed() (flight_mech.plane.Plane method) compute_temperature_from_altitude() (flight_mech.atmosphere.StandardAtmosphere static method) compute_thrust() (flight_mech.plane.Plane method) compute_thrust_needed() (flight_mech.plane.Plane method) compute_v_at_gliding_v_z_min() (flight_mech.plane.Plane method) compute_velocity_interval_for_fixed_thrust() (flight_mech.plane.Plane method) compute_zero_lift_drag() (flight_mech.wing.Wing method) compute_zero_lift_drag_on_wing_slice() (flight_mech.wing.Wing method) ConstantAtmosphere (class in flight_mech.atmosphere) convert_float_or_none_to_string() (in module flight_mech.airfoil) convert_theta_to_y() (in module flight_mech.wing) convert_y_to_theta() (in module flight_mech.wing) create_3D_animation() (flight_mech.wing.Wing method) create_wing_3D_surface() (flight_mech.wing.Wing method) current_OPR (flight_mech.turbine.TurbojetSingleBody attribute) D density (flight_mech.fuel.FuelModel attribute) DIESEL (flight_mech.fuel.FuelTable attribute) download_web_file() (in module flight_mech.airfoil) E efficiency (flight_mech.motor.ElectricalMotor property) ElectricalMotor (class in flight_mech.motor) electromotive_force (flight_mech.motor.ElectricalMotor property) engine_type (flight_mech.plane.Plane attribute) environment_model (flight_mech.plane.Plane attribute) extension (flight_mech.plane.Plane property) external_resistance (flight_mech.motor.ElectricalMotor attribute) extrados_z_array (flight_mech.airfoil.Airfoil attribute) F f() (flight_mech.plane.Plane method) f_max (flight_mech.plane.Plane property) flight_mech module flight_mech.aerodynamics module flight_mech.airfoil module flight_mech.atmosphere module flight_mech.fuel module flight_mech.motor module flight_mech.plane module flight_mech.turbine module flight_mech.wing module fuel_consumption (flight_mech.turbine.TurbojetSingleBody property) fuel_specific_conso (flight_mech.plane.Plane attribute) fuel_specific_conso_SI (flight_mech.plane.Plane property) FuelModel (class in flight_mech.fuel) FuelTable (class in flight_mech.fuel) G gas_model (flight_mech.atmosphere.AtmosphereModel attribute) (flight_mech.atmosphere.ConstantAtmosphere attribute) (flight_mech.atmosphere.LinearAtmosphere attribute) (flight_mech.atmosphere.StandardAtmosphere attribute) gas_models module GASOLINE (flight_mech.fuel.FuelTable attribute) get_chord_incidence() (flight_mech.airfoil.Airfoil method) get_rotated_selig_arrays() (flight_mech.airfoil.Airfoil method) global_efficiency (flight_mech.turbine.TurbojetSingleBody property) ground_effect_coefficient (flight_mech.plane.Plane attribute) H H2 (flight_mech.fuel.FuelTable attribute) I I (flight_mech.motor.ElectricalMotor property) I_0 (flight_mech.motor.ElectricalMotor attribute) I_max (flight_mech.motor.ElectricalMotor attribute) import_from_airfoiltools() (flight_mech.airfoil.Airfoil method) import_xz_selig_arrays() (flight_mech.airfoil.Airfoil method) initialize() (flight_mech.wing.Wing method) internal_resistance (flight_mech.motor.ElectricalMotor attribute) intrados_z_array (flight_mech.airfoil.Airfoil attribute) J JET_A (flight_mech.fuel.FuelTable attribute) JP_4 (flight_mech.fuel.FuelTable attribute) JP_5 (flight_mech.fuel.FuelTable attribute) K k (flight_mech.plane.Plane attribute) KEROSENE (flight_mech.fuel.FuelTable attribute) Kv (flight_mech.motor.ElectricalMotor attribute) L leading_edge_x_array (flight_mech.wing.Wing property) LinearAtmosphere (class in flight_mech.atmosphere) list_airfoils_in_database() (flight_mech.airfoil.Airfoil method) load_database_airfoil() (flight_mech.airfoil.Airfoil method) load_motor_data() (flight_mech.motor.ElectricalMotor method) load_plane_data() (flight_mech.plane.Plane method) load_selig_file() (flight_mech.airfoil.Airfoil method) lower_heating_value (flight_mech.fuel.FuelModel attribute) M m (flight_mech.plane.Plane property) M8 (flight_mech.turbine.TurbojetSingleBody property) m_empty (flight_mech.plane.Plane attribute) m_fuel (flight_mech.plane.Plane attribute) m_payload (flight_mech.plane.Plane attribute) mass (flight_mech.motor.ElectricalMotor attribute) max_camber (flight_mech.airfoil.Airfoil property) max_camber_location (flight_mech.airfoil.Airfoil property) max_efficiency (flight_mech.motor.ElectricalMotor property) max_reference_surface_mass_flow_rate_4_star (flight_mech.turbine.TurbojetSingleBody attribute) max_thickness (flight_mech.airfoil.Airfoil property) max_thickness_location (flight_mech.airfoil.Airfoil property) METHANE (flight_mech.fuel.FuelTable attribute) module flight_mech flight_mech.aerodynamics flight_mech.airfoil flight_mech.atmosphere flight_mech.fuel flight_mech.motor flight_mech.plane flight_mech.turbine flight_mech.wing gas_models N n() (flight_mech.plane.Plane method) naca_airfoil_generator() (in module flight_mech.airfoil) name (flight_mech.airfoil.Airfoil attribute) (flight_mech.wing.Wing attribute) nb_engines (flight_mech.plane.Plane attribute) O OPR_design (flight_mech.turbine.TurbojetSingleBody attribute) P P (flight_mech.plane.Plane attribute) P0 (flight_mech.turbine.TurbojetSingleBody property) P1 (flight_mech.turbine.TurbojetSingleBody property) P2 (flight_mech.turbine.TurbojetSingleBody property) P3 (flight_mech.turbine.TurbojetSingleBody property) P4 (flight_mech.turbine.TurbojetSingleBody property) P5 (flight_mech.turbine.TurbojetSingleBody property) P8 (flight_mech.turbine.TurbojetSingleBody property) Plane (class in flight_mech.plane) plot() (flight_mech.airfoil.Airfoil method) plot_2D() (flight_mech.wing.Wing method) plot_3D() (flight_mech.wing.Wing method) plot_CL_graph() (flight_mech.airfoil.Airfoil method) plot_Cm_graph() (flight_mech.airfoil.Airfoil method) plot_gliding_TV_graph() (flight_mech.plane.Plane method) plot_gliding_WV_graph() (flight_mech.plane.Plane method) plot_graph() (flight_mech.atmosphere.AtmosphereModel method) (flight_mech.motor.ElectricalMotor method) plot_polar_graph() (flight_mech.plane.Plane method) power (flight_mech.motor.ElectricalMotor property) propulsive_efficiency (flight_mech.turbine.TurbojetSingleBody property) Ps8 (flight_mech.turbine.TurbojetSingleBody property) R re_interpolate() (flight_mech.airfoil.Airfoil method) (flight_mech.wing.Wing method) re_interpolate_with_cosine_distribution() (flight_mech.airfoil.Airfoil method) reference_surface (flight_mech.wing.Wing property) rotate_arrays() (in module flight_mech.airfoil) rotation_speed (flight_mech.motor.ElectricalMotor property) S S (flight_mech.plane.Plane attribute) save_3D_shape() (flight_mech.wing.Wing method) set_at_max_efficiency() (flight_mech.motor.ElectricalMotor method) set_chord_at_zero_incidence() (flight_mech.airfoil.Airfoil method) set_motor_parameters() (flight_mech.motor.ElectricalMotor method) set_plane_parameters() (flight_mech.plane.Plane method) single_side_surface (flight_mech.wing.Wing property) StandardAtmosphere (class in flight_mech.atmosphere) sweep_angle_at_leading_edge (flight_mech.wing.Wing property) sweep_angle_at_trailing_edge (flight_mech.wing.Wing property) T T0 (flight_mech.turbine.TurbojetSingleBody property) T1 (flight_mech.turbine.TurbojetSingleBody property) T2 (flight_mech.turbine.TurbojetSingleBody property) T3 (flight_mech.turbine.TurbojetSingleBody property) T4 (flight_mech.turbine.TurbojetSingleBody property) T4_instruction (flight_mech.turbine.TurbojetSingleBody property) T4_max (flight_mech.turbine.TurbojetSingleBody attribute) T5 (flight_mech.turbine.TurbojetSingleBody property) T8 (flight_mech.turbine.TurbojetSingleBody property) taper_ratio (flight_mech.wing.Wing property) thermal_efficiency (flight_mech.turbine.TurbojetSingleBody property) thickness_array (flight_mech.airfoil.Airfoil property) thrust (flight_mech.turbine.TurbojetSingleBody property) thrust_per_engine (flight_mech.plane.Plane attribute) torque (flight_mech.motor.ElectricalMotor property) trailing_edge_x_array (flight_mech.wing.Wing property) Ts8 (flight_mech.turbine.TurbojetSingleBody property) tune_A4_star_for_desired_thrust() (flight_mech.turbine.TurbojetSingleBody method) tune_current_OPR() (flight_mech.turbine.TurbojetSingleBody method) turbine_efficiency (flight_mech.turbine.TurbojetSingleBody attribute) TurbojetSingleBody (class in flight_mech.turbine) twisting_angle_array (flight_mech.wing.Wing attribute) U U (flight_mech.motor.ElectricalMotor property) U_max (flight_mech.motor.ElectricalMotor attribute) update_C_L_max() (flight_mech.plane.Plane method) update_gas_model_to_altitude_conditions() (flight_mech.atmosphere.StandardAtmosphere class method) update_ground_effect_coefficient() (flight_mech.plane.Plane method) update_k() (flight_mech.plane.Plane method) update_P() (flight_mech.plane.Plane method) update_variables() (flight_mech.plane.Plane method) V v() (flight_mech.plane.Plane method) V0 (flight_mech.turbine.TurbojetSingleBody property) V8 (flight_mech.turbine.TurbojetSingleBody property) W W0 (flight_mech.turbine.TurbojetSingleBody property) W1 (flight_mech.turbine.TurbojetSingleBody property) W2 (flight_mech.turbine.TurbojetSingleBody property) W3 (flight_mech.turbine.TurbojetSingleBody property) W4 (flight_mech.turbine.TurbojetSingleBody property) W4R (flight_mech.turbine.TurbojetSingleBody property) W5 (flight_mech.turbine.TurbojetSingleBody property) W8 (flight_mech.turbine.TurbojetSingleBody property) W8R (flight_mech.turbine.TurbojetSingleBody property) Wf (flight_mech.turbine.TurbojetSingleBody property) Wing (class in flight_mech.wing) wing_shape_coefficient (flight_mech.plane.Plane attribute) wing_span (flight_mech.wing.Wing property) wing_to_ground_height (flight_mech.plane.Plane attribute) X x_array (flight_mech.airfoil.Airfoil property) x_center_offset_array (flight_mech.wing.Wing attribute) x_selig_array (flight_mech.airfoil.Airfoil property) Y y_array (flight_mech.wing.Wing property) Z z_selig_array (flight_mech.airfoil.Airfoil property)