Index _ | A | B | C | D | E | F | G | H | I | J | K | L | M | N | O | P | Q | R | S | T | V | W | X | Y _ _compute_area_z_str() (tuduam.structures.wingbox.IdealWingbox method) _compute_boom_areas() (tuduam.structures.wingbox.IdealWingbox method) _evaluate() (tuduam.structures.optimization.ProblemFixedPanel method) (tuduam.structures.optimization.ProblemFreePanel method) _kb_interp() (tuduam.structures.constraints.IsotropicWingboxConstraints method) _n_col() (tuduam.structures.constraints.IsotropicWingboxConstraints method) _read_skin_panels_per_cell (tuduam.structures.wingbox.IdealWingbox property) _set_Ixx() (tuduam.structures.wingbox.IdealWingbox method) _set_Ixy() (tuduam.structures.wingbox.IdealWingbox method) _set_Iyy() (tuduam.structures.wingbox.IdealWingbox method) A a_fac() (tuduam.propulsion.OffDesignAnalysisBEM method) a_prim_fac() (tuduam.propulsion.OffDesignAnalysisBEM method) alpha_xfoil_interp() (in module tuduam.propulsion) alpha_zero_lift (tuduam.data_structures.Aerodynamics attribute) analyse_propeller() (tuduam.propulsion.OffDesignAnalysisBEM method) area_str (tuduam.data_structures.Wingbox attribute) aspect_ratio (tuduam.data_structures.SingleWing attribute) B battery_mass (tuduam.data_structures.HybridPowertrain attribute) BEM (class in tuduam.propulsion) beta_crippling (tuduam.data_structures.Material attribute) Boom (class in tuduam.structures.wingbox) C cd0 (tuduam.data_structures.Aerodynamics attribute) cd_xfoil_interp() (in module tuduam.propulsion) chord_arr (tuduam.data_structures.Propeller attribute) chord_mac (tuduam.data_structures.SingleWing attribute) chord_root (tuduam.data_structures.SingleWing attribute) chord_tip (tuduam.data_structures.SingleWing attribute) cL_alpha (tuduam.data_structures.Aerodynamics attribute) cl_alpha (tuduam.data_structures.Airfoil attribute) cL_cruise (tuduam.data_structures.FlightPerformance attribute) cl_xfoil_interp() (in module tuduam.propulsion) class2_fuselage_mass() (in module tuduam.mass_metrics) class2_wing_mass() (in module tuduam.mass_metrics) column_str_buckling() (tuduam.structures.constraints.IsotropicWingboxConstraints method) component_drag() (in module tuduam.aerodynamics) compute_direct_stress() (tuduam.structures.wingbox.IdealWingbox method) crippling() (tuduam.structures.constraints.IsotropicWingboxConstraints method) crit_instability_compr() (tuduam.structures.constraints.IsotropicWingboxConstraints method) crit_instability_shear() (tuduam.structures.constraints.IsotropicWingboxConstraints method) Cx() (tuduam.propulsion.OffDesignAnalysisBEM method) Cy() (tuduam.propulsion.OffDesignAnalysisBEM method) D density (tuduam.data_structures.Material attribute) density() (tuduam.performance.ISA method) diameter (tuduam.data_structures.Engine attribute) discretize_airfoil() (in module tuduam.structures.wingbox) drag_coefficient() (in module tuduam.aerodynamics) E eff() (tuduam.propulsion.OffDesignAnalysisBEM method) efficiency() (tuduam.propulsion.BEM method) extract_data_dir() (in module tuduam.propulsion) F F() (tuduam.propulsion.BEM method) f() (tuduam.propulsion.BEM method) F() (tuduam.propulsion.OffDesignAnalysisBEM method) f() (tuduam.propulsion.OffDesignAnalysisBEM method) F_int() (tuduam.propulsion.BEM method) f_int() (tuduam.propulsion.BEM method) fl_thickness (tuduam.data_structures.SingleWing attribute) fuel_cell_mass (tuduam.data_structures.HybridPowertrain attribute) full_section_opt() (tuduam.structures.optimization.SectionOpt method) G g_crippling (tuduam.data_structures.Material attribute) G_int() (tuduam.propulsion.BEM method) GA_optimize() (tuduam.structures.optimization.SectionOpt method) get_cell_areas() (tuduam.structures.wingbox.IdealWingbox method) get_cell_idx() (tuduam.structures.wingbox.Boom method) (tuduam.structures.wingbox.IdealPanel method) get_centroids() (in module tuduam.structures.wingbox) get_polygon_cells() (tuduam.structures.wingbox.IdealWingbox method) get_total_area() (tuduam.structures.wingbox.IdealWingbox method) global_skin_buckling() (tuduam.structures.constraints.IsotropicWingboxConstraints method) H h_cruise (tuduam.data_structures.FlightPerformance attribute) h_st (tuduam.data_structures.Wingbox attribute) height_fuselage (tuduam.data_structures.Fuselage attribute) I I_prim_1() (tuduam.propulsion.BEM method) I_prim_2() (tuduam.propulsion.BEM method) IdealPanel (class in tuduam.structures.wingbox) IdealWingbox (class in tuduam.structures.wingbox) ignore_loc (tuduam.data_structures.Engine attribute) interaction_curve() (tuduam.structures.constraints.IsotropicWingboxConstraints method) ISA (class in tuduam.performance) IsotropicWingboxConstraints (class in tuduam.structures.constraints) J J() (tuduam.propulsion.BEM method) J_prim_1() (tuduam.propulsion.BEM method) J_prim_2() (tuduam.propulsion.BEM method) K K() (tuduam.propulsion.OffDesignAnalysisBEM method) K_prim() (tuduam.propulsion.OffDesignAnalysisBEM method) L l_function() (in module tuduam.aerodynamics) length() (tuduam.structures.wingbox.IdealPanel method) length_fuselage (tuduam.data_structures.Fuselage attribute) lift_curve_slope() (in module tuduam.aerodynamics) lift_distribution() (in module tuduam.aerodynamics) load_airfoil() (tuduam.propulsion.PlotBlade method) load_factor (tuduam.data_structures.Material attribute) load_from_json() (tuduam.data_structures.Parent class method) load_new_gauge() (tuduam.structures.wingbox.IdealWingbox method) M M() (tuduam.propulsion.BEM method) (tuduam.propulsion.OffDesignAnalysisBEM method) m_crippling (tuduam.data_structures.Material attribute) mass (tuduam.data_structures.Engine attribute) (tuduam.data_structures.Fuselage attribute) (tuduam.data_structures.SingleWing attribute) mission_energy (tuduam.data_structures.FlightPerformance attribute) module tuduam.aerodynamics tuduam.data_structures tuduam.mass_metrics tuduam.performance tuduam.propulsion tuduam.structures.wingbox mtom (tuduam.data_structures.VTOL attribute) N n_blades (tuduam.data_structures.Propeller attribute) n_cell (tuduam.data_structures.Wingbox attribute) n_engines (tuduam.data_structures.Engine attribute) n_ribs (tuduam.data_structures.SingleWing attribute) n_str (tuduam.data_structures.SingleWing attribute) n_ult (tuduam.data_structures.FlightPerformance attribute) O oem (tuduam.data_structures.VTOL attribute) OffDesignAnalysisBEM (class in tuduam.propulsion) optimise_blade() (tuduam.propulsion.BEM method) optimize_cobyla() (tuduam.structures.optimization.SectionOpt method) P PG() (tuduam.propulsion.BEM method) PG_correct() (tuduam.propulsion.OffDesignAnalysisBEM method) phi() (tuduam.propulsion.BEM method) (tuduam.propulsion.OffDesignAnalysisBEM method) phi_int() (tuduam.propulsion.BEM method) phi_t() (tuduam.propulsion.BEM method) pitch_arr (tuduam.data_structures.Propeller attribute) planform_geometry() (in module tuduam.aerodynamics) plot_3D() (tuduam.propulsion.PlotBlade method) plot_3D_plotly() (tuduam.propulsion.PlotBlade method) plot_blade() (tuduam.propulsion.PlotBlade method) plot_direct_stresses() (tuduam.structures.wingbox.IdealWingbox method) plot_geometry() (tuduam.structures.wingbox.IdealWingbox method) plot_quiver_shear_stress() (tuduam.structures.wingbox.IdealWingbox method) plot_shear_stress() (tuduam.structures.wingbox.IdealWingbox method) PlotBlade (class in tuduam.propulsion) poisson (tuduam.data_structures.Material attribute) post_buckling_ratio (tuduam.data_structures.Material attribute) power_grav_density (tuduam.data_structures.Engine attribute) power_vol_density (tuduam.data_structures.Engine attribute) pressure() (tuduam.performance.ISA method) ProblemFixedPanel (class in tuduam.structures.optimization) ProblemFreePanel (class in tuduam.structures.optimization) Q quarterchord_sweep (tuduam.data_structures.SingleWing attribute) R r_prop (tuduam.data_structures.Propeller attribute) rad_arr (tuduam.data_structures.Propeller attribute) read_coord() (in module tuduam.structures.wingbox) rib_loc (tuduam.data_structures.SingleWing attribute) RN() (tuduam.propulsion.BEM method) (tuduam.propulsion.OffDesignAnalysisBEM method) rpm_cruise (tuduam.data_structures.Propeller attribute) run_BEM() (tuduam.propulsion.BEM method) S safety_factor (tuduam.data_structures.Material attribute) SectionOpt (class in tuduam.structures.optimization) set_b1_to_b2_vector() (tuduam.structures.wingbox.IdealPanel method) set_b2_to_b1_vector() (tuduam.structures.wingbox.IdealPanel method) shear_modulus (tuduam.data_structures.Material attribute) shear_strength (tuduam.data_structures.Material attribute) sigma_ultimate (tuduam.data_structures.Material attribute) sigma_yield (tuduam.data_structures.Material attribute) skin_thickness (tuduam.data_structures.SingleWing attribute) solidity_local() (tuduam.propulsion.OffDesignAnalysisBEM method) soundspeed() (tuduam.performance.ISA method) span (tuduam.data_structures.SingleWing attribute) spanwise_points (tuduam.data_structures.Aerodynamics attribute) spar_loc_nondim (tuduam.data_structures.Wingbox attribute) spar_thickness (tuduam.data_structures.SingleWing attribute) spline_airfoil_coord() (in module tuduam.structures.wingbox) str_cell (tuduam.data_structures.Wingbox attribute) stress_analysis() (tuduam.structures.wingbox.IdealWingbox method) stringer_flange_buckling() (tuduam.structures.constraints.IsotropicWingboxConstraints method) stringer_height (tuduam.data_structures.SingleWing attribute) stringer_thickness (tuduam.data_structures.SingleWing attribute) stringer_web_buckling() (tuduam.structures.constraints.IsotropicWingboxConstraints method) stringer_width (tuduam.data_structures.SingleWing attribute) surface (tuduam.data_structures.SingleWing attribute) sweep_le (tuduam.data_structures.SingleWing attribute) T t_rib (tuduam.data_structures.SingleWing attribute) t_sk_cell (tuduam.data_structures.Wingbox attribute) t_sp (tuduam.data_structures.Wingbox attribute) t_st (tuduam.data_structures.Wingbox attribute) taper (tuduam.data_structures.SingleWing attribute) tc_ratio (tuduam.data_structures.Propeller attribute) temperature() (tuduam.performance.ISA method) thickness_to_chord (tuduam.data_structures.Airfoil attribute) thrust (tuduam.data_structures.Engine attribute) tuduam.aerodynamics module tuduam.data_structures module tuduam.mass_metrics module tuduam.performance module tuduam.propulsion module tuduam.structures.wingbox module V v_cruise (tuduam.data_structures.FlightPerformance attribute) viscosity_dyn() (tuduam.performance.ISA method) von_Mises() (tuduam.structures.constraints.IsotropicWingboxConstraints method) W W() (tuduam.propulsion.OffDesignAnalysisBEM method) w_st (tuduam.data_structures.Wingbox attribute) washout (tuduam.data_structures.SingleWing attribute) Wc() (tuduam.propulsion.BEM method) weissinger_l() (in module tuduam.aerodynamics) width_fuselage (tuduam.data_structures.Fuselage attribute) wingbox_end (tuduam.data_structures.SingleWing attribute) wingbox_start (tuduam.data_structures.SingleWing attribute) wingloading (tuduam.data_structures.FlightPerformance attribute) X x() (tuduam.propulsion.BEM method) x_le_root_global (tuduam.data_structures.SingleWing attribute) x_lemac_local (tuduam.data_structures.SingleWing attribute) x_rotor_loc (tuduam.data_structures.Engine attribute) x_rotor_rel_loc (tuduam.data_structures.Engine attribute) Xi() (tuduam.propulsion.BEM method) (tuduam.propulsion.OffDesignAnalysisBEM method) xi_0 (tuduam.data_structures.Propeller attribute) Y y_mac (tuduam.data_structures.SingleWing attribute) y_rotor_loc (tuduam.data_structures.Engine attribute) young_modulus (tuduam.data_structures.Material attribute)