def zero_all_text_fields(self):
try:
profile_, surfaceType_, 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_x_, section_2_x_, section_3_x_, section_4_x_, section_5_x_, \
section_1_y_, section_2_y_, section_3_y_, section_4_y_, section_5_y_, \
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_twist_angle_, section_2_twist_angle_, \
section_3_twist_angle_, section_4_twist_angle_, section_5_twist_angle_ = read_surface_data(self._name)
self.show_default_values(
profile_=profile_,
surfaceType_=surfaceType_,
xz_mirror_=xz_mirror_,
xy_mirror_=xy_mirror_,
yz_mirror_=yz_mirror_,
rot_x_=rot_x_,
rot_y_=rot_y_,
rot_z_=rot_z_,
root_le_pos_x_=root_le_pos_x_,
root_le_pos_y_=root_le_pos_y_,
root_le_pos_z_=root_le_pos_z_,
section_1_x_=section_1_x_,
section_2_x_=section_2_x_,
section_3_x_=section_3_x_,
section_4_x_=section_4_x_,
section_5_x_=section_5_x_,
section_1_y_=section_1_y_,
section_2_y_=section_2_y_,
section_3_y_=section_3_y_,
section_4_y_=section_4_y_,
section_5_y_=section_5_y_,
section_1_z_=section_1_z_,
section_2_z_=section_2_z_,
section_3_z_=section_3_z_,
section_4_z_=section_4_z_,
section_5_z_=section_5_z_,
section_1_chord_=section_1_chord_,
section_2_chord_=section_2_chord_,
section_3_chord_=section_3_chord_,
section_4_chord_=section_4_chord_,
section_5_chord_=section_5_chord_,
section_1_twist_angle_=section_1_twist_angle_,
section_2_twist_angle_=section_2_twist_angle_,
section_3_twist_angle_=section_3_twist_angle_,
section_4_twist_angle_=section_4_twist_angle_,
section_5_twist_angle_=section_5_twist_angle_)
except:
self.show_default_values()
def zero_all_text_fields(self):
try:
root_location_x, root_location_y, root_location_z, dihedral, sweep, twist, span, taper_ratio, chord, winglet_width, winglet_rotation, winglet_center_translation_x, winglet_center_translation_y, winglet_center_translation_z, profile = \
read_surface_data(self.text)
self.show_default_values(
root_location_x=root_location_x,
root_location_y=root_location_y,
root_location_z=root_location_z,
dihedral=dihedral,
sweep=sweep,
twist=twist,
span=span,
taper_ratio=taper_ratio,
chord=chord,
winglet_width=winglet_width,
winglet_rotation=winglet_rotation,
winglet_center_translation_x=winglet_center_translation_x,
winglet_center_translation_y=winglet_center_translation_y,
winglet_center_translation_z=winglet_center_translation_z,
profile=profile)
except:
self.show_default_values()
def zero_all_text_fields(self):
try:
root_location_x, root_location_y, root_location_z, dihedral, sweep, twist, span, taper_ratio, chord, profile = read_surface_data(
self.text)
self.show_default_values(root_location_x=root_location_x,
root_location_y=root_location_y,
root_location_z=root_location_z,
dihedral=dihedral,
sweep=sweep,
twist=twist,
span=span,
taper_ratio=taper_ratio,
chord=chord,
profile=profile)
except (Exception):
self.show_default_values()
def read_parameters(self):
try:
self.airfoil_type, self.surfaceType_, self.xz_mirror_, self.xy_mirror_, self.yz_mirror_, self.rot_x_, self.rot_y_, self.rot_z_, self.root_le_pos_x_, self.root_le_pos_y_, self.root_le_pos_z_, \
self.section_1_x_, self.section_2_x_, self.section_3_x_, self.section_4_x_, self.section_5_x_, \
self.section_1_y_, self.section_2_y_, self.section_3_y_, self.section_4_y_, self.section_5_y_, \
self.section_1_z_, self.section_2_z_, self.section_3_z_, self.section_4_z_, self.section_5_z_, \
self.section_1_chord_, self.section_2_chord_, self.section_3_chord_, self.section_4_chord_, \
self.section_5_chord_, self.section_1_twist_angle_, self.section_2_twist_angle_, \
self.section_3_twist_angle_, self.section_4_twist_angle_, self.section_5_twist_angle_ = read_surface_data(
self._name)
except (Exception):
self.airfoil_type = "naca0012"
def read_parameters(self):
self.root_location_x, self.root_location_y, self.root_location_z, self.dihedral, \
self.sweep, self.twist, self.span, self.taper_ratio, \
self.chord, self.profile = read_surface_data(
self._name)
def read_parameters(self):
self.root_location_x, self.root_location_y, self.root_location_z, self.dihedral, \
self.sweep, self.twist, self.span, self.taper_ratio, \
self.chord, self.winglet_width, self.winglet_rotation, self.winglet_center_translation_x, \
self.winglet_center_translation_y, self.winglet_center_translation_z, self.profile = read_surface_data(
self._name)
