def update_boom_3D(workflow=None):
boom_list = read_boom_objects()
for l in boom_list:
design_type_, boom_type_ = get_boom_object_data(l)
generate_boom_3D_model(workflow,
name=l,
boom_type_=boom_type_,
design_type_=design_type_)
def update_boom_3d(config=None):
boom_list = read_boom_objects()
lofts = {}
try:
for l in boom_list:
design_type_, boom_type_ = get_boom_object_data(l)
lofts.update({
l:
generate_boom_3D_model(config,
name=l,
boom_type_=boom_type_,
design_type_=design_type_)
})
except:
pass
return lofts
def load_booms(self):
try:
boom_list = read_boom_objects()
if len(boom_list) == 0:
self.new_boom()
for l in boom_list:
design_type_, boom_type_ = get_boom_object_data(l)
if design_type_ == unconventional_design:
self.boom_tab_ = boom_tab(l, boom_type_, design_type_)
self.booms.append(self.boom_tab_)
self.booms.append(self.boom_tab_)
self.inputArea.addTab(self.boom_tab_, l)
self.indexes.append(l)
elif design_type_ == conventional_design:
self.boom_tab_ = fuselage_tab(l, boom_type_, design_type_)
self.booms.append(self.boom_tab_)
self.booms.append(self.boom_tab_)
self.inputArea.addTab(self.boom_tab_, l)
self.indexes.append(l)
except:
self.new_boom()
def get_booms():
try:
boom_list = read_boom_objects()
fuselages = []
for l in boom_list:
design_type_, surface_type_ = get_boom_object_data(l)
xsecs = []
root_position_x_, root_position_y_, root_position_z_ = 0, 0, 0
xz_mirror_ = False
if design_type_ == conventional_design:
radii, x, z, root_position_x_, root_position_y_, root_position_z_, xz_mirror_ = get_parameters_for_fuselage(
l)
for radius, x_, z_ in zip(radii, x, z):
xsecs.append(
FuselageXSec(x_c=x_, y_c=0, z_c=z_, radius=radius))
fuselages.append(
Fuselage(name=l,
x_le=root_position_x_,
y_le=root_position_y_,
z_le=root_position_z_,
symmetric=xz_mirror_,
xsecs=xsecs))
elif design_type_ == unconventional_design:
radii, x, z, root_position_x_, root_position_y_, root_position_z_, xz_mirror_ = get_parameters_for_boom(
l)
for radius, x_, z_ in zip(radii, x, z):
xsecs.append(
FuselageXSec(x_c=x_, y_c=0, z_c=z_, radius=radius))
fuselages.append(
Fuselage(name=l,
x_le=root_position_x_,
y_le=root_position_y_,
z_le=root_position_z_,
symmetric=xz_mirror_,
xsecs=xsecs))
return fuselages
except:
return []
def build_datcom_input():
surface_list = read_lifting_surface_objects()
ls_statements = []
boom_statements = []
synths={}
for l in surface_list:
design_type_, surface_type_ = get_surface_object_data(l)
span_, tip_chord, root_chord, dihedral_, sweep_ = 0, 0, 0, 0, 0
profile_="0012"
if design_type_ == unconventional_design:
span_, tip_chord, root_chord, dihedral_, sweep_,profile_ = get_parameters_from_sections_lifting_surface(l)
elif design_type_ == conventional_design:
print(l)
span_, tip_chord, root_chord, dihedral_, sweep_,profile_ = get_parameters_from_conventional_wing(l)
print(profile_.split("naca"))
if surface_type_ == wing:
synths.update({"wing": span_ / 2})
ls_statements.append(set_planform_parameters(
type_1="W,G", tip_chord=tip_chord,
root_chord=root_chord, semi_span=(span_ / 2), sweep_angle=sweep_,
dihedral_=1.2,
profile=profile_.split("naca")[1]
))
elif surface_type_ == fin:
synths.update({"vtp":span_ / 2})
ls_statements.append(set_planform_parameters(
type_1="V,T", tip_chord=tip_chord,
root_chord=root_chord, semi_span=(span_ / 2), sweep_angle=sweep_,
dihedral_=1.3,
profile=profile_.split("naca")[1]
))
else:
synths.update({"vtp": span_ / 2})
ls_statements.append(set_planform_parameters(
type_1="H,T", tip_chord=tip_chord,
root_chord=root_chord, semi_span=(span_ / 2), sweep_angle=sweep_,
dihedral_=1.3,
profile=profile_.split("naca")[1]
))
try:
boom_list = read_boom_objects()
for l in boom_list:
design_type_, surface_type_ = get_boom_object_data(l)
if design_type_ == unconventional_design:
pass
elif design_type_ == conventional_design:
radii, x, z = get_parameters_from_conventional_boom(l)
boom_statements.append(set_body_parameters_radius(section_positions=x, radius_of_sections=radii,
iter_=(boom_list.index(l) + 1)))
except:
pass
mesh = get_center_of_mass()
try:
value=synths["vtp"]
except:
synths.update({"vtp":0})
try:
value=synths["htp"]
except:
synths.update({"htp":0})
input_ = "".join([set_flight_conditions(mach_numbers=get_mach_number(), angle_of_attack=get_aoa_range(), altitude=get_altitude()),
set_synths_parameters(center_of_gravity_x=round(mesh["x"],2),center_of_gravity_z=round(mesh["z"],2),
vtp_tip_position_x=round(synths.get("vtp"),2),
htp_tip_position_x=round(synths.get("htp"),2)),
"".join(ls_statements),
"".join(boom_statements),
create_footer()])
database.write_datcom_input(input=input_)