Index

A

airfoil (airfoil_db.DatabaseBoundsError attribute)

airfoil_db (module)

B

Battery (class in pyprop)

battery (pyprop.PropulsionUnit attribute) BladeElementProp (class in pyprop)

C

calc_batt_life() (pyprop.PropulsionUnit method) calc_cruise_throttle() (pyprop.PropulsionUnit method) calc_cruise_thrust() (pyprop.PropulsionUnit method) calc_motor_torque() (pyprop.PropulsionUnit method)

command (pyprop.DatabaseRecordNotFoundError attribute) component_name (pyprop.MaxCurrentExceededError attribute) component_type (pyprop.MaxCurrentExceededError attribute) create_component_from_database() (in module pyprop)

D

DatabaseBoundsError (class in airfoil_db) DatabaseDataProp (class in pyprop) DatabaseFitProp (class in pyprop)

DatabaseRecordNotFoundError (class in pyprop) diameter (pyprop.BladeElementProp attribute) (pyprop.DatabaseDataProp attribute) (pyprop.DatabaseFitProp attribute)

E

error_type (pyprop.ThrottleNotFoundError attribute) ESC (class in pyprop)

esc (pyprop.PropulsionUnit attribute) exception_indices (airfoil_db.DatabaseBoundsError attribute)

F

final_val (pyprop.ThrottleNotFoundError attribute)

G

get_advance_ratio() (pyprop.BladeElementProp method) (pyprop.DatabaseDataProp method) (pyprop.DatabaseFitProp method) get_diameter() (pyprop.BladeElementProp method) (pyprop.DatabaseDataProp method) (pyprop.DatabaseFitProp method) get_electric_power() (pyprop.PropulsionUnit method) get_power_coef() (pyprop.BladeElementProp method) (pyprop.DatabaseDataProp method) (pyprop.DatabaseFitProp method)

get_thrust_coef() (pyprop.BladeElementProp method) (pyprop.DatabaseDataProp method) (pyprop.DatabaseFitProp method) get_torque_coef() (pyprop.BladeElementProp method) (pyprop.DatabaseDataProp method) (pyprop.DatabaseFitProp method) get_velocity() (pyprop.BladeElementProp method) (pyprop.DatabaseDataProp method) (pyprop.DatabaseFitProp method) get_weight() (pyprop.PropulsionUnit method)

I

I_drawn (pyprop.MaxCurrentExceededError attribute) I_max (pyprop.MaxCurrentExceededError attribute)

I_motor (pyprop.PropulsionUnit attribute) inputs_dict (airfoil_db.DatabaseBoundsError attribute) InvalidRuntimeError (class in pyprop)

J

J (pyprop.PropDataBoundsError attribute)

K

k (pyprop.BladeElementProp attribute)

M

MaxCurrentExceededError (class in pyprop) message (airfoil_db.DatabaseBoundsError attribute)

Motor (class in pyprop) motor (pyprop.PropulsionUnit attribute)

N

name (pyprop.BladeElementProp attribute)

O

Optimizer (class in pyprop)

P

pitch (pyprop.DatabaseDataProp attribute) (pyprop.DatabaseFitProp attribute) plot_angles_over_zeta() (pyprop.BladeElementProp method) plot_coefs() (pyprop.BladeElementProp method) (pyprop.DatabaseDataProp method) (pyprop.DatabaseFitProp method)

plot_thrust_curves() (pyprop.PropulsionUnit method) prop (pyprop.PropDataBoundsError attribute) (pyprop.PropulsionUnit attribute) PropDataBoundsError (class in pyprop) PropulsionUnit (class in pyprop) pyprop (module), [1], [2], [3], [4], [5], [6], [7], [8]

R

random_search() (pyprop.Optimizer method)

rpm (pyprop.PropDataBoundsError attribute) runtime (pyprop.InvalidRuntimeError attribute)

T

T_req (pyprop.ThrottleNotFoundError attribute) throttle (pyprop.TorquesNotMatchedError attribute) ThrottleNotFoundError (class in pyprop)

to_rads() (in module pyprop) to_rpm() (in module pyprop) TorquesNotMatchedError (class in pyprop)

V

v_cruise (pyprop.ThrottleNotFoundError attribute) (pyprop.TorquesNotMatchedError attribute)

W

weight (pyprop.BladeElementProp attribute) write_to_database() (pyprop.Battery method) (pyprop.ESC method) (pyprop.Motor method)