def get_current_loft(self):
wires = []
curves = []
propeller_number_, xz_mirror_, xy_mirror_, yz_mirror_ \
, rot_x_, hub_length, pitch_angle, 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_ = read_propeller_parameters(
name=self.name)
interval = 5
chords = [
section_1_chord_, section_1_chord_, section_2_chord_,
section_3_chord_, section_4_chord_, section_5_chord_, 0.001
]
profile = [
section_1_profile_, section_1_profile_, section_2_profile_,
section_3_profile_, section_4_profile_, section_5_profile_,
section_5_profile_
]
length = [
0, section_1_length_, section_2_length_, section_3_length_,
section_4_length_, section_5_length_ / 2, section_5_length_ / 2
]
z = [
section_1_z_, section_1_z_, section_2_z_, section_3_z_,
section_4_z_, section_5_z_, section_5_z_
]
pitch = [
0, section_1_pitch_angle_, section_2_pitch_angle_,
section_3_pitch_angle_, section_4_pitch_angle_,
section_5_pitch_angle_, section_5_pitch_angle_
]
n = random.random()
lifting_surface = self.config.get_wings().create_wing(
f"{n}", len(chords), f"naca4412")
sections = [-hub_length / 2, 0.1 * hub_length, hub_length / 2]
radius = [
0.00,
rot_x_ / 2,
rot_x_ / 2,
]
x_ = []
x_.extend(np.linspace(sections[0], sections[1], num=interval))
x_.append(0.9 * hub_length)
radii = []
radii.extend(np.linspace(radius[0], radius[1], num=interval))
radii.append((rot_x_ / 2))
print(x_, radii)
n = random.random()
hub = self.config.get_fuselages().create_fuselage(
f"hub{n}", len(x_), "circularProfile")
for (x, rad, index) in zip(x_, radii, range(1, len(x_) + 1)):
section = hub.get_section(index)
sectionElement = section.get_section_element(1)
sectionElementCenter = sectionElement.get_ctigl_section_element()
sectionElementCenter.set_center(tigl3.geometry.CTiglPoint(x, 0, 0))
sectionElementCenter.set_area(getArea(rad))
n_sections = lifting_surface.get_section_count()
lifting_surface.set_root_leposition(
tigl3.geometry.CTiglPoint(-chords[0] / 2, 0, 0))
print(n_sections)
y = 0.0
x = hub_length / 2
for (z_, chord, length_, pitch_, profile_,
idx) in zip(z, chords, length, pitch, profile,
range(1, n_sections + 1)):
profile__ = "naca" + profile_
constant = 0.0
nacanumber = profile__.split("naca")[1]
if nacanumber.isdigit():
if len(nacanumber) == 4:
constant = int(nacanumber[2:]) * 0.01
s = lifting_surface.get_section(idx)
e = s.get_section_element(1)
ce = e.get_ctigl_section_element()
ce.set_width(chord)
ce.set_height(chord * constant)
center = ce.get_center()
y += length_
center.x = x
center.y = y
center.z = 0.0
ce.set_center(center)
ce.set_profile_uid(f"{profile_}")
e.set_rotation(tigl3.geometry.CTiglPoint(0, pitch_, 0))
lifting_surface.set_rotation(
tigl3.geometry.CTiglPoint(0, pitch_angle, 0))
for idx in range(1, n_sections + 1):
s = lifting_surface.get_section(idx)
e = s.get_section_element(1)
ce = e.get_ctigl_section_element()
wires.append(ce.get_wire())
for l in wires:
adapt = BRepAdaptor_CompCurve(l)
curve = Handle_BRepAdaptor_HCompCurve(
BRepAdaptor_HCompCurve(adapt))
approx = Approx_Curve3d(curve, 0.001, GeomAbs_C2, 200, 12)
if (approx.IsDone() and approx.HasResult()):
curves.append(approx.Curve())
surface1 = tigl3.surface_factories.interpolate_curves(curves)
face1 = BRepBuilderAPI_MakeFace(surface1, 1e-6).Face()
face2 = BRepBuilderAPI_MakeFace(surface1, 1e-6).Face()
sew = BRepBuilderAPI_Sewing()
sew.Add(face1)
sew.Add(face2)
sew.Perform()
shape = sew.SewedShape()
print(shape)
tds = topods()
model = BRepBuilderAPI_MakeSolid()
model.Add(tds.Shell(shape))
solid = model.Solid()
print(solid)
rot_trafo = tigl3.geometry.CTiglTransformation()
rot_trafo.add_rotation_x(90)
loft = []
loft.append(hub.get_loft().shape())
loft.append(
tigl3.geometry.CNamedShape(rot_trafo.transform(solid),
"cut").shape())
if propeller_number_ == 2:
trafo = tigl3.geometry.CTiglTransformation()
trafo.add_mirroring_at_xzplane()
loft.append(
tigl3.geometry.CNamedShape(trafo.transform(loft[1]),
"cut").shape())
elif propeller_number_ >= 3:
delta = 360 / propeller_number_
for i in range(1, propeller_number_ + 1):
loft_copy = deepcopy(loft[1])
trafo = tigl3.geometry.CTiglTransformation()
trafo.add_rotation_x(delta * i)
print(delta * i)
loft.append(
tigl3.geometry.CNamedShape(trafo.transform(loft_copy),
"cut").shape())
builder = BRep_Builder()
assembly = TopoDS_Compound()
builder.MakeCompound(assembly)
for l in loft:
builder.Add(assembly, l)
trafo = tigl3.geometry.CTiglTransformation()
trafo.add_translation(root_le_pos_x_, root_le_pos_y_, root_le_pos_z_)
assembly = trafo.transform(assembly)
return [assembly]
def make_solid_from_shell_list(occ_shell_list):
ms = BRepBuilderAPI_MakeSolid()
for occ_shell in occ_shell_list:
ms.Add(occ_shell)
return ms.Solid()
def curved_surface(self):
self.read_parameters()
n = random.random()
self.lifting_surface = self.wings.create_wing(f"{n}", 5,
self.airfoil_type)
chords = [
self.section_1_chord_, self.section_2_chord_,
self.section_3_chord_, self.section_4_chord_, self.section_5_chord_
]
y = [
self.section_1_y_, self.section_2_y_, self.section_3_y_,
self.section_4_y_, self.section_5_y_
]
x = [
self.section_1_x_, self.section_2_x_, self.section_3_x_,
self.section_4_x_, self.section_5_x_
]
z = [
self.section_1_z_, self.section_2_z_, self.section_3_z_,
self.section_4_z_, self.section_5_z_
]
twist = [
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_
]
profile = self.airfoil_type
constant = 0.5
nacanumber = profile.split("naca")[1]
if nacanumber.isdigit():
if len(nacanumber) == 4:
constant = int(nacanumber[2:]) * 0.01
# decrease section size towards wing tips
wires = []
curves = []
n_sections = self.lifting_surface.get_section_count()
for idx in range(1, n_sections + 1):
s = self.lifting_surface.get_section(idx)
e = s.get_section_element(1)
ce = e.get_ctigl_section_element()
ce.set_width(chords[idx - 1])
ce.set_height(chords[idx - 1] * constant)
center = ce.get_center()
center.x = x[idx - 1]
center.y = y[idx - 1]
center.z = z[idx - 1]
ce.set_center(center)
self.lifting_surface.set_rotation(
tigl3.geometry.CTiglPoint(self.rot_x_, self.rot_y_, self.rot_z_))
self.lifting_surface.set_root_leposition(
tigl3.geometry.CTiglPoint(self.root_le_pos_x_, self.root_le_pos_y_,
self.root_le_pos_z_))
for idx in range(1, n_sections + 1):
s = self.lifting_surface.get_section(idx)
e = s.get_section_element(1)
ce = e.get_ctigl_section_element()
wires.append(ce.get_wire())
for l in wires:
adapt = BRepAdaptor_CompCurve(l)
curve = Handle_BRepAdaptor_HCompCurve(
BRepAdaptor_HCompCurve(adapt))
approx = Approx_Curve3d(curve, 0.001, GeomAbs_C2, 200, 12)
if (approx.IsDone() and approx.HasResult()):
curves.append(approx.Curve())
surface = tigl3.surface_factories.interpolate_curves(curves)
sew = BRepBuilderAPI_Sewing()
face1 = BRepBuilderAPI_MakeFace(surface, 1e-6).Face()
face2 = BRepBuilderAPI_MakeFace(surface, 1e-6).Face()
sew.Add(face1)
sew.Add(face2)
sew.Perform()
shape = sew.SewedShape()
tds = topods()
model = BRepBuilderAPI_MakeSolid()
model.Add(tds.Shell(shape))
solid = model.Solid()
loft = []
loft.append(solid)
if self.xy_mirror_:
trafo = tigl3.geometry.CTiglTransformation()
trafo.add_mirroring_at_xyplane()
loft.append(
tigl3.geometry.CNamedShape(trafo.transform(loft[0]),
"cut").shape())
elif self.xz_mirror_:
trafo = tigl3.geometry.CTiglTransformation()
trafo.add_mirroring_at_xzplane()
loft.append(
tigl3.geometry.CNamedShape(trafo.transform(loft[0]),
"cut").shape())
elif self.yz_mirror_:
trafo = tigl3.geometry.CTiglTransformation()
trafo.add_mirroring_at_yzplane()
loft.append(
tigl3.geometry.CNamedShape(trafo.transform(loft[0]),
"cut").shape())
self.old_profile = self.airfoil_type
return loft
def make_solid(occ_shell):
ms = BRepBuilderAPI_MakeSolid()
ms.Add(occ_shell)
return ms.Solid()