def delete_propeller_objects(value=""):
data = database.read_propulsion_specifications()
try:
array = data[propeller_objects]
array.remove(value)
data[propeller_objects] = array
except:
pass
database.write_propulsion_specifications(data)
def read_propulsion_parameters():
values = database.read_propulsion_specifications()
values = values[propulsion]
voltage_ = values[voltage]
max_thrust_ = values[max_thrust]
battery_capacity_ = values[battery_capacity]
discharge_rate_ = values[discharge_rate]
max_current_ = values[max_current]
return voltage_, max_thrust_, battery_capacity_, discharge_rate_, max_current_
def read_propeller_parameters(name):
values = database.read_propulsion_specifications()[propeller][name]
if values is None:
values = {}
propeller_number_ = values[propeller_number]
rot_x_ = values[rotation_x]
rot_y_ = values[rotation_y]
rot_z_ = values[pitch_angle]
root_le_pos_x_ = values[hub_position_x]
root_le_pos_y_ = values[hub_position_y]
root_le_pos_z_ = values[hub_position_z]
xz_mirror_ = values.get(xz_mirror)
xy_mirror_ = values.get(xy_mirror)
yz_mirror_ = values.get(yz_mirror)
section_1_chord_ = values[section_1_chord]
section_1_length_ = values[section_1_length]
section_1_profile_ = values[section_1_profile]
section_1_z_ = values[section_1_z]
section_1_pitch_angle_ = values[section_1_pitch_angle]
section_2_chord_ = values[section_2_chord]
section_2_length_ = values[section_2_length]
section_2_profile_ = values[section_2_profile]
section_2_z_ = values[section_2_z]
section_2_pitch_angle_ = values[section_2_pitch_angle]
section_3_chord_ = values[section_3_chord]
section_3_length_ = values[section_3_length]
section_3_profile_ = values[section_3_profile]
section_3_z_ = values[section_3_z]
section_3_pitch_angle_ = values[section_3_pitch_angle]
section_4_chord_ = values[section_4_chord]
section_4_length_ = values[section_4_length]
section_4_profile_ = values[section_4_profile]
section_4_z_ = values[section_4_z]
section_4_pitch_angle_ = values[section_4_pitch_angle]
section_5_chord_ = values[section_5_chord]
section_5_length_ = values[section_5_length]
section_5_profile_ = values[section_5_profile]
section_5_z_ = values[section_5_z]
section_5_pitch_angle_ = values[section_5_pitch_angle]
return propeller_number_, xz_mirror_, xy_mirror_, yz_mirror_ \
, rot_x_, rot_y_, rot_z_, root_le_pos_x_, \
root_le_pos_y_, root_le_pos_z_, section_1_length_, section_2_length_, \
section_3_length_, section_4_length_, section_5_length_, section_1_profile_, \
section_2_profile_, section_3_profile_, section_4_profile_, section_5_profile_, \
section_1_z_, section_2_z_, section_3_z_, section_4_z_, section_5_z_ \
, section_1_chord_, section_2_chord_, section_3_chord_, section_4_chord_, \
section_5_chord_, section_1_pitch_angle_, section_2_pitch_angle_, \
section_3_pitch_angle_, section_4_pitch_angle_, section_5_pitch_angle_
def write_propeller_objects(value=""):
data = database.read_propulsion_specifications()
try:
array = data[propeller_objects]
if not array.__contains__(value):
array.append(value)
data[propeller_objects] = array
except Exception as e:
logging.error(e)
data.update({propeller_objects: [value]})
database.write_propulsion_specifications(data)
def read_shroud_parameters():
values = database.read_propulsion_specifications()[propeller][shroud]
if values is None:
values = {}
shroud_inner_diameter_ = values[shroud_inner_diameter]
shroud_outer_diameter_ = values[shroud_outer_diameter]
shroud_length_ = values[shroud_length]
shroud_taper_ratio_ = values[shroud_taper_ratio]
shroud_number_ = values[shroud_number]
root_le_pos_x_ = values[hub_position_x]
root_le_pos_y_ = values[hub_position_y]
root_le_pos_z_ = values[hub_position_z]
xz_mirror_ = values.get(xz_mirror)
xy_mirror_ = values.get(xy_mirror)
yz_mirror_ = values.get(yz_mirror)
return shroud_length_, root_le_pos_x_, root_le_pos_y_, root_le_pos_z_, shroud_number_, shroud_taper_ratio_, shroud_inner_diameter_, shroud_outer_diameter_, xy_mirror_, xz_mirror_, yz_mirror_
def exportValues():
output = ""
for major_key in database.read_datcom_stability_specifications().keys():
for key in database.read_datcom_stability_specifications(
)[major_key].keys():
alpha_, velocity_, y = read_datcom_table_data(type_=datcom_data,
major_key=major_key,
key=key)
try:
value = y[alpha_.index(0)]
except:
value = 0
output = output + f"{key}:{value},"
for key, value in database.read_propulsion_specifications(
)["propulsion_dialogs"].items():
output = output + f"{key}:{value},"
for key, value in database.read_structures_specifications().items():
try:
for k, v in value.items():
output = output + f"{k}:{v},"
except:
output = output + f"{key}:{value},"
writeTxt(sim_export_txt_dir, output)
def read_propeller_objects():
data = database.read_propulsion_specifications()
return data[propeller_objects]