Index

_

_predict_derivatives() (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilModel method)

_predict_values() (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilModel method) _process_polar_parameters() (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilModel method)

A

a_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) ac_states (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) AircaftStates (class in BladeAD.utils.var_groups) alpha_stall_minus (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute) alpha_stall_plus (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute)

angular_speed_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) are_all_elements_of_type() (in module BladeAD.core.airfoil.composite_airfoil_model) atmos_states (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) AtmosStates (class in BladeAD.utils.var_groups) axial_induced_velocity (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) azimuth_angle_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute)

B

bem_residual (BladeAD.core.BEM.compute_inflow_angle.ImplicitModelOutputs attribute) BEMModel (class in BladeAD.core.BEM.bem_model) BladeAD.core module BladeAD.core.airfoil module BladeAD.core.airfoil.composite_airfoil_model module BladeAD.core.airfoil.zero_d_airfoil_model module BladeAD.core.airfoil.zero_d_airfoil_model_custom_op module BladeAD.core.BEM module BladeAD.core.BEM.bem_model module BladeAD.core.BEM.compute_inflow_angle module BladeAD.core.BEM.compute_quantities_of_interest module BladeAD.core.peters_he module BladeAD.core.peters_he.peters_he_inflow module BladeAD.core.peters_he.peters_he_model module BladeAD.core.pitt_peters module BladeAD.core.pitt_peters.pitt_peters_inflow module

BladeAD.core.pitt_peters.pitt_peters_model module BladeAD.core.preprocessing module BladeAD.core.preprocessing.compute_local_frame_velocity module BladeAD.core.preprocessing.preprocess_variables module BladeAD.utils module BladeAD.utils.define_rotor_analysis module BladeAD.utils.integration_schemes module BladeAD.utils.parameterization module BladeAD.utils.parameterization_custom_op module BladeAD.utils.plot module BladeAD.utils.smooth_quantities_spanwise module BladeAD.utils.switching_fun module BladeAD.utils.var_groups module BladeAD.utils.verify_dynamic_inflow_models_plotting module BsplineParameterization (class in BladeAD.utils.parameterization) BSplineParameterizationExplicitOperation (class in BladeAD.utils.parameterization_custom_op) build_model_from_parameters() (in module two_d_airfoil_model)

C

Cd (BladeAD.core.BEM.compute_inflow_angle.ImplicitModelOutputs attribute) Cd_0 (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute) Cd_model (NACA_4412.naca_4412_model.NACA4412MLAirfoilModel attribute) Cd_reg (in module NACA_4412.naca_4412_model) Cd_stall_minus (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute) Cd_stall_plus (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute) chord_profile (BladeAD.utils.var_groups.RotorMeshParameters attribute) chord_profile_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) Cl (BladeAD.core.BEM.compute_inflow_angle.ImplicitModelOutputs attribute) Cl_0 (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute) Cl_alpha (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute) Cl_model (NACA_4412.naca_4412_model.NACA4412MLAirfoilModel attribute) Cl_reg (in module NACA_4412.naca_4412_model) Cl_stall_minus (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute) Cl_stall_plus (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilPolarParameters attribute)

CompositeAirfoilModel (class in BladeAD.core.airfoil.composite_airfoil_model) compute() (BladeAD.core.airfoil.zero_d_airfoil_model_custom_op.ZeroDAirfoilCustomOperation method) (BladeAD.utils.parameterization_custom_op.BSplineParameterizationExplicitOperation method) (NACA_4412.naca_4412_model.NACA4412MLAirfoilModelCustomOperation method) (two_d_airfoil_model.TwoDMLAirfoilModelCustomOp method) compute_derivatives() (BladeAD.core.airfoil.zero_d_airfoil_model_custom_op.ZeroDAirfoilCustomOperation method) (BladeAD.utils.parameterization_custom_op.BSplineParameterizationExplicitOperation method) (NACA_4412.naca_4412_model.NACA4412MLAirfoilModelCustomOperation method) (two_d_airfoil_model.TwoDMLAirfoilModelCustomOp method) compute_gamma() (in module BladeAD.core.peters_he.peters_he_inflow) compute_h() (in module BladeAD.core.peters_he.peters_he_inflow) compute_inflow_angle() (in module BladeAD.core.BEM.compute_inflow_angle) compute_L() (in module BladeAD.core.peters_he.peters_he_inflow) compute_local_frame_velocities() (in module BladeAD.core.preprocessing.compute_local_frame_velocity) compute_phi() (in module BladeAD.core.peters_he.peters_he_inflow) compute_quantities_of_interest() (in module BladeAD.core.BEM.compute_quantities_of_interest)

D

define_model() (in module two_d_airfoil_model) density (BladeAD.utils.var_groups.AtmosStates attribute) device (in module NACA_4412.naca_4412_model) (in module two_d_airfoil_model)

df (in module BladeAD.core.peters_he.peters_he_inflow) disk_inclination_angle (BladeAD.core.preprocessing.compute_local_frame_velocity.LocalFrameVelocities attribute) double_factorial() (in module BladeAD.core.peters_he.peters_he_inflow) dynamic_viscosity (BladeAD.utils.var_groups.AtmosStates attribute)

E

efficiency (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) element_width (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) evaluate() (BladeAD.core.airfoil.composite_airfoil_model.CompositeAirfoilModel method) (BladeAD.core.airfoil.zero_d_airfoil_model.ZeroDAirfoilModel method) (BladeAD.core.airfoil.zero_d_airfoil_model_custom_op.ZeroDAirfoilCustomOperation method) (BladeAD.core.BEM.bem_model.BEMModel method) (BladeAD.core.peters_he.peters_he_model.PetersHeModel method) (BladeAD.core.pitt_peters.pitt_peters_model.PittPetersModel method) (BladeAD.utils.parameterization_custom_op.BSplineParameterizationExplicitOperation method) (NACA_4412.naca_4412_model.NACA4412MLAirfoilModel method) (NACA_4412.naca_4412_model.NACA4412MLAirfoilModelCustomOperation method) (two_d_airfoil_model.TwoDMLAirfoilModel method) (two_d_airfoil_model.TwoDMLAirfoilModelCustomOp method)

evaluate_radial_profile() (BladeAD.utils.parameterization.BsplineParameterization method)

F

figure_of_merit (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute)

forces (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute)

G

get_bspline_mtx() (in module BladeAD.utils.parameterization)

get_ml_model() (in module two_d_airfoil_model)

H

hub_radius (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute)

I

ImplicitModelOutputs (class in BladeAD.core.BEM.compute_inflow_angle) inflow_angle (BladeAD.core.BEM.compute_inflow_angle.ImplicitModelOutputs attribute)

integrate_quantity() (in module BladeAD.utils.integration_schemes) is_ascending_between_0_and_1() (in module BladeAD.core.airfoil.composite_airfoil_model)

L

local_frame_velocity (BladeAD.core.preprocessing.compute_local_frame_velocity.LocalFrameVelocities attribute)

LocalFrameVelocities (class in BladeAD.core.preprocessing.compute_local_frame_velocity)

M

make_polarplot() (in module BladeAD.utils.plot) mesh_parameters (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) mesh_velocity (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) module BladeAD.core BladeAD.core.airfoil BladeAD.core.airfoil.composite_airfoil_model BladeAD.core.airfoil.zero_d_airfoil_model BladeAD.core.airfoil.zero_d_airfoil_model_custom_op BladeAD.core.BEM BladeAD.core.BEM.bem_model BladeAD.core.BEM.compute_inflow_angle BladeAD.core.BEM.compute_quantities_of_interest BladeAD.core.peters_he BladeAD.core.peters_he.peters_he_inflow BladeAD.core.peters_he.peters_he_model BladeAD.core.pitt_peters BladeAD.core.pitt_peters.pitt_peters_inflow BladeAD.core.pitt_peters.pitt_peters_model BladeAD.core.preprocessing BladeAD.core.preprocessing.compute_local_frame_velocity BladeAD.core.preprocessing.preprocess_variables BladeAD.utils BladeAD.utils.define_rotor_analysis BladeAD.utils.integration_schemes BladeAD.utils.parameterization BladeAD.utils.parameterization_custom_op BladeAD.utils.plot BladeAD.utils.smooth_quantities_spanwise BladeAD.utils.switching_fun BladeAD.utils.var_groups BladeAD.utils.verify_dynamic_inflow_models_plotting NACA_4412 NACA_4412.naca_4412_model two_d_airfoil_model

moments (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) mu (BladeAD.core.preprocessing.compute_local_frame_velocity.LocalFrameVelocities attribute) mu_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) mu_z (BladeAD.core.preprocessing.compute_local_frame_velocity.LocalFrameVelocities attribute)

N

NACA4412MLAirfoilModel (class in NACA_4412.naca_4412_model) NACA4412MLAirfoilModelCustomOperation (class in NACA_4412.naca_4412_model) NACA_4412 module NACA_4412.naca_4412_model module

norm_hub_radius (BladeAD.utils.var_groups.RotorMeshParameters attribute) norm_radius_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) num_azimuthal (BladeAD.utils.var_groups.RotorMeshParameters attribute) num_blades (BladeAD.utils.var_groups.RotorMeshParameters attribute) num_radial (BladeAD.utils.var_groups.RotorMeshParameters attribute)

P

p (BladeAD.utils.var_groups.AircaftStates attribute) PetersHeModel (class in BladeAD.core.peters_he.peters_he_model) phi (BladeAD.utils.var_groups.AircaftStates attribute) PittPetersModel (class in BladeAD.core.pitt_peters.pitt_peters_model) plot_vnv_data() (in module BladeAD.utils.verify_dynamic_inflow_models_plotting)

power_coefficient (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) preprocess_input_variables() (in module BladeAD.core.preprocessing.preprocess_variables) PreProcessOutputs (class in BladeAD.core.preprocessing.preprocess_variables) pressure (BladeAD.utils.var_groups.AtmosStates attribute) psi (BladeAD.utils.var_groups.AircaftStates attribute)

Q

q (BladeAD.utils.var_groups.AircaftStates attribute)

R

r (BladeAD.utils.var_groups.AircaftStates attribute) radius (BladeAD.utils.var_groups.RotorMeshParameters attribute) radius_vector_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) recorder (in module NACA_4412.naca_4412_model) (in module two_d_airfoil_model) residual (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute)

rho_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) RotorAnalysisInputs (class in BladeAD.utils.var_groups) RotorAnalysisOutputs (class in BladeAD.utils.var_groups) RotorMeshParameters (class in BladeAD.utils.var_groups) rpm (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) run_rotor_analysis() (in module BladeAD.utils.define_rotor_analysis)

S

sectional_drag (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) sectional_inflow_angle (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) sectional_thrust (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) sectional_torque (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) sigma (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute)

sigmoid() (in module BladeAD.utils.switching_fun) smooth_quantities_spanwise() (in module BladeAD.utils.smooth_quantities_spanwise) solve_for_steady_state_inflow() (in module BladeAD.core.peters_he.peters_he_inflow) (in module BladeAD.core.pitt_peters.pitt_peters_inflow) speed_of_sound (BladeAD.utils.var_groups.AtmosStates attribute)

T

tangential_induced_velocity (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) tangential_velocity (BladeAD.core.preprocessing.compute_local_frame_velocity.LocalFrameVelocities attribute) temperature (BladeAD.utils.var_groups.AtmosStates attribute) theta (BladeAD.utils.var_groups.AircaftStates attribute) theta_0 (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) theta_1_c (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) theta_1_s (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) thrust_coefficient (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) thrust_origin (BladeAD.utils.var_groups.RotorMeshParameters attribute) thrust_origin_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) thrust_origin_vel_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) thrust_vector (BladeAD.utils.var_groups.RotorMeshParameters attribute)

thrust_vector_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) tip_loss_factor (BladeAD.core.BEM.compute_inflow_angle.ImplicitModelOutputs attribute) torque_coefficient (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) total_power (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) total_thrust (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) total_torque (BladeAD.utils.var_groups.RotorAnalysisOutputs attribute) train_two_d_airfoil_model() (in module two_d_airfoil_model) twist_profile (BladeAD.utils.var_groups.RotorMeshParameters attribute) twist_profile_exp (BladeAD.core.preprocessing.preprocess_variables.PreProcessOutputs attribute) two_d_airfoil_model module TwoDMLAirfoilModel (class in two_d_airfoil_model) TwoDMLAirfoilModelCustomOp (class in two_d_airfoil_model)

U

u (BladeAD.utils.var_groups.AircaftStates attribute)

V

v (BladeAD.utils.var_groups.AircaftStates attribute)

W

w (BladeAD.utils.var_groups.AircaftStates attribute)

X

x (BladeAD.utils.var_groups.AircaftStates attribute) (in module BladeAD.utils.switching_fun)

xi_0 (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) xi_1_c (BladeAD.utils.var_groups.RotorAnalysisInputs attribute) xi_1_s (BladeAD.utils.var_groups.RotorAnalysisInputs attribute)

Y

y (BladeAD.utils.var_groups.AircaftStates attribute)

Z

z (BladeAD.utils.var_groups.AircaftStates attribute) ZeroDAirfoilCustomOperation (class in BladeAD.core.airfoil.zero_d_airfoil_model_custom_op)

ZeroDAirfoilModel (class in BladeAD.core.airfoil.zero_d_airfoil_model) ZeroDAirfoilPolarParameters (class in BladeAD.core.airfoil.zero_d_airfoil_model)