def test_beam_offset(self):
bm1 = Beam(
"bm1",
n1=[0, 0, 0],
n2=[2, 0, 0],
sec="IPE300",
mat=Material("SteelMat", CarbonSteel("S420")),
colour="red",
up=(0, 0, 1),
e1=(0, 0, -0.1),
e2=(0, 0, -0.1),
)
bm2 = Beam(
"bm2",
n1=[0, 0, 0],
n2=[2, 0, 0],
sec="IPE300",
mat=Material("SteelMat", CarbonSteel("S420")),
colour="blue",
up=(0, 0, -1),
e1=(0, 0, -0.1),
e2=(0, 0, -0.1),
)
a = Assembly("Toplevel") / [Part("MyPart") / [bm1, bm2]]
a.to_ifc(test_folder / "beams_offset.ifc")
def read_material(ifc_mat, ifc_ref: "IfcRef",
assembly: "Assembly") -> Material:
from ada.materials.metals import CarbonSteel, Metal
mat_psets = ifc_mat.HasProperties if hasattr(ifc_mat,
"HasProperties") else None
if mat_psets is None or len(mat_psets) == 0:
logging.info(f'No material properties found for "{ifc_mat}"')
return Material(ifc_mat.Name)
props = {}
for entity in mat_psets[0].Properties:
if entity.is_a("IfcPropertySingleValue"):
props[entity.Name] = entity.NominalValue[0]
mat_props = dict(
E=props.get("YoungModulus", 210000e6),
sig_y=props.get("YieldStress", 355e6),
rho=props.get("MassDensity", 7850),
v=props.get("PoissonRatio", 0.3),
alpha=props.get("ThermalExpansionCoefficient", 1.2e-5),
zeta=props.get("SpecificHeatCapacity", 1.15),
units=assembly.units,
)
if "StrengthGrade" in props:
mat_model = CarbonSteel(grade=props["StrengthGrade"], **mat_props)
else:
mat_model = Metal(sig_u=None, **mat_props)
return Material(name=ifc_mat.Name,
mat_model=mat_model,
ifc_ref=ifc_ref,
units=assembly.units)
def test_main_properties():
matS355 = Material("MatS355", mat_model=CarbonSteel("S355"))
matS420 = Material("MatS420", mat_model=CarbonSteel("S420"))
for model in [matS355.model, matS420.model]:
assert model.E == 2.1e11
assert model.rho == 7850
assert model.v == 0.3
assert matS355.model.sig_y == 355e6
assert matS420.model.sig_y == 420e6
def test_bm():
bm = Beam("MyBeam", (0, 0.5, 0.5), (5, 0.5, 0.5), "IPE400", Material("S420", CarbonSteel("S420")))
f1 = fundamental_eigenfrequency(bm)
f2 = 6.268 * f1
f3 = 17.456 * f1
print(f"Fundamental Eigenfrequencies\n\n1: {f1}\n2: {f2}\n3: {f3}")
return bm
def get_morsmel(m):
"""
MORSMEL
Anisotropy, Linear Elastic Structural Analysis, 2-D Membrane Elements and 2-D Thin Shell Elements
:param m:
:return:
"""
d = m.groupdict()
matno = str_to_int(d["matno"])
return Material(
name=mat_names[matno],
mat_id=matno,
mat_model=CarbonSteel(
rho=roundoff(d["rho"]),
E=roundoff(d["d11"]),
v=roundoff(d["ps1"]),
alpha=roundoff(d["alpha1"]),
zeta=roundoff(d["damp1"]),
sig_p=[],
eps_p=[],
sig_y=5e6,
),
metadata=d,
parent=part,
)
def beam_ex1(p1=(0, 0, 0), p2=(1.5, 0, 0), profile="IPE400"):
"""
:return:
:rtype: ada.Assembly
"""
bm = Beam("MyBeam", p1, p2, profile, Material("S355"))
a = Assembly("Test", user=User("krande")) / [Part("MyPart") / bm]
h = 0.2
r = 0.02
normal = [0, 1, 0]
xdir = [-1, 0, 0]
# Polygon Extrusions
origin = np.array([0.2, -0.1, -0.1])
points = [(0, 0), (0.1, 0), (0.05, 0.1)]
bm.add_penetration(PrimExtrude("Poly1", points, h, normal, origin, xdir))
origin += np.array([0.2, 0, 0])
points = [(0, 0, r), (0.1, 0, r), (0.05, 0.1, r)]
bm.add_penetration(PrimExtrude("Poly2", points, h, normal, origin, xdir))
origin += np.array([0.2, 0, 0])
points = [(0, 0, r), (0.1, 0, r), (0.1, 0.2, r), (0.0, 0.2, r)]
bm.add_penetration(PrimExtrude("Poly3", points, h, normal, origin, xdir))
# Cylinder Extrude
x = origin[0] + 0.2
bm.add_penetration(PrimCyl("cylinder", (x, -0.1, 0), (x, 0.1, 0), 0.1))
# Box Extrude
x += 0.2
bm.add_penetration(PrimBox("box", (x, -0.1, -0.1), (x + 0.2, 0.1, 0.1)))
# Create a FEM analysis of the beam as a cantilever subjected to gravity loads
p = a.get_part("MyPart")
create_beam_mesh(bm, p.fem, "shell")
# Add a set containing ALL elements (necessary for Calculix loads).
fs = p.fem.add_set(FemSet("Eall", [el for el in p.fem.elements], "elset"))
step = a.fem.add_step(
Step("gravity",
"static",
nl_geom=True,
init_incr=100.0,
total_time=100.0))
step.add_load(Load("grav", "gravity", -9.81 * 800, fem_set=fs))
fix_set = p.fem.add_set(FemSet("bc_nodes", get_beam_end_nodes(bm), "nset"))
a.fem.add_bc(Bc("Fixed", fix_set, [1, 2, 3]))
return a
def mat_from_list(mat_int, mat_str):
guid, name, units = str_fix(mat_str)
E, rho, sigy = mat_int
return Material(name=name,
guid=guid,
units=units,
mat_model=CarbonSteel(E=E, rho=rho, sig_y=sigy),
parent=parent)
def mat_str_to_mat_obj(mat_str):
"""
Converts a Abaqus materials str into a ADA Materials object
:param mat_str:
:return:
"""
from ada import Material
rd = roundoff
# Name
name = re.search(r"name=(.*?)\n", mat_str, _re_in).group(1).split("=")[-1].strip()
# Density
density_ = re.search(r"\*Density\n(.*?)(?:,|$)", mat_str, _re_in)
if density_ is not None:
density = rd(density_.group(1).strip().split(",")[0].strip(), 10)
else:
print('No density flag found for material "{}"'.format(name))
density = None
# Elastic
re_elastic_ = re.search(r"\*Elastic(?:,\s*type=(.*?)|)\n(.*?)(?:\*|$)", mat_str, _re_in)
if re_elastic_ is not None:
re_elastic = re_elastic_.group(2).strip().split(",")
young, poisson = rd(re_elastic[0]), rd(re_elastic[1])
else:
print('No Elastic properties found for material "{name}"'.format(name=name))
young, poisson = None, None
# Plastic
re_plastic_ = re.search(r"\*Plastic\n(.*?)(?:\*|\Z)", mat_str, _re_in)
if re_plastic_ is not None:
re_plastic = [tuple(x.split(",")) for x in re_plastic_.group(1).strip().splitlines()]
sig_p = [rd(x[0]) for x in re_plastic]
eps_p = [rd(x[1]) for x in re_plastic]
else:
eps_p, sig_p = None, None
# Expansion
re_zeta = re.search(r"\*Expansion(?:,\s*type=(.*?)|)\n(.*?)(?:\*|$)", mat_str, _re_in)
if re_zeta is not None:
zeta = float(re_zeta.group(2).split(",")[0].strip())
else:
zeta = 0.0
# Return material object
model = CarbonSteel(
rho=density,
E=young,
v=poisson,
eps_p=eps_p,
zeta=zeta,
sig_p=sig_p,
plasticity_model=None,
)
return Material(name=name, mat_model=model)
def test_material_ifc_roundtrip(materials_test_dir):
ifc_path = materials_test_dir / "my_material.ifc"
p = Part("MyPart")
p.add_material(Material("my_mat"))
a = Assembly("MyAssembly") / p
fp = a.to_ifc(ifc_path, return_file_obj=True)
b = ada.from_ifc(fp)
assert len(b.materials) == 1
def test_material_equal(self):
matvar = dict(
sec_type="IG",
h=0.8,
w_top=0.2,
w_btn=0.2,
t_fbtn=0.01,
t_ftop=0.01,
t_w=0.01,
)
Material("MyMat")
def test_material_ifc_roundtrip(self):
ifc_name = "my_material.ifc"
a = Assembly("MyAssembly")
p = Part("MyPart")
p.add_material(Material("my_mat"))
a.add_part(p)
a.to_ifc(test_folder / ifc_name)
b = Assembly("MyImport")
b.read_ifc(test_folder / ifc_name)
def test_negative_sec_contained(self):
# A minor change in section box thickness
sec = Section("myBG", from_str="BG800x400x20x40")
mat = Material("my_mat")
bm = Beam("my_beam", (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], "B31")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec", "beam", fem_set, mat, sec)
p = get_fsec_bm_collection()
self.assertFalse(fem_sec in p.fem.sections)
def test_material_ifc_roundtrip(self):
ifc_name = 'my_material.ifc'
a = Assembly('MyAssembly')
p = Part('MyPart')
p.add_material(Material('my_mat'))
a.add_part(p)
a.to_ifc(test_folder / ifc_name)
b = Assembly('MyImport')
b.read_ifc(test_folder / ifc_name)
def test_negative_sec_contained(self):
# A minor change in section box thickness
sec = Section('myBG', from_str='BG800x400x20x40')
mat = Material('my_mat')
bm = Beam('my_beam', (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], 'B31')
fem_set = FemSet('my_set', [elem], 'elset')
fem_sec = FemSection('my_sec', 'beam', fem_set, mat, sec)
p = get_fsec_bm_collection()
self.assertFalse(fem_sec in p.fem.sections)
def test_negative_mat_contained(self):
# A minor change in material property (S420 instead of S355)
sec = Section('myBG', from_str='BG800x400x30x40')
mat = Material('my_mat', CarbonSteel('S420'))
bm = Beam('my_beam', (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], 'B31')
fem_set = FemSet('my_set', [elem], 'elset')
fem_sec = FemSection('my_sec', 'beam', fem_set, mat, sec)
p = get_fsec_bm_collection()
self.assertFalse(fem_sec in p.fem.sections)
def part_with_beam():
sec = Section("myIPE", from_str="BG800x400x30x40")
mat = Material("my_mat")
bm = Beam("my_beam", (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], "line")
p = Part("my_part") / bm
fem_set = p.fem.sets.add(FemSet("my_set", [elem]))
p.fem.sections.add(
FemSection("my_sec", "line", fem_set, mat, sec, local_z=(0, 0, 1)))
p.fem.elements.add(elem)
return p
def test_negative_mat_contained(self):
# A minor change in material property (S420 instead of S355)
sec = Section("myBG", from_str="BG800x400x30x40")
mat = Material("my_mat", CarbonSteel("S420"))
bm = Beam("my_beam", (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], "B31")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec", "beam", fem_set, mat, sec)
p = get_fsec_bm_collection()
self.assertFalse(fem_sec in p.fem.sections)
def test_negative_contained_shell_(part_with_shell):
# Testing equal operator for change in element type
mat = Material("my_mat")
elem = Elem(
1,
[Node((0, 0, 0)),
Node((1, 0, 0)),
Node((1, 1, 0)),
Node((0, 1, 0))], "quad")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec", "shell", fem_set, mat, thickness=0.01)
assert fem_sec not in part_with_shell.fem.sections
def test_merge_materials():
plates = []
for i in range(1, 10):
mat = Material(f"mat{i}", CarbonSteel("S355"))
plates.append(
Plate(f"pl{i}", [(0, 0, 0), (0, 1, 0), (1, 1, 0)], 20e-3, mat=mat))
a = Assembly() / (Part("MyPart") / plates)
p = a.get_part("MyPart")
mats = p.materials
assert len(mats) == 9
mats.merge_materials_by_properties()
assert len(mats) == 1
def create_ifc(name, up=(0, 0, 1)):
a = Assembly("MyAssembly")
p = Part(name)
p.add_beam(
Beam(
"bm_up",
n1=[0, 0, 0],
n2=[2, 0, 0],
sec="HP200x10",
mat=Material("SteelMat", CarbonSteel("S420")),
colour="red",
up=up,
))
a.add_part(p)
a.to_ifc(test_folder / name)
def test_negative_contained_shell_(self):
# Testing equal operator for change in element type
mat = Material("my_mat")
elem = Elem(1, [
Node((0, 0, 0)),
Node((1, 0, 0)),
Node((1, 1, 0)),
Node((0, 1, 0))
], "S4")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec", "shell", fem_set, mat, thickness=0.01)
p = get_fsec_sh_collection()
self.assertFalse(fem_sec in p.fem.sections)
def test_negative_contained_shell(self):
# Testing equal operator for different shell thickness
mat = Material('my_mat')
elem = Elem(1, [
Node((0, 0, 0)),
Node((1, 0, 0)),
Node((1, 1, 0)),
Node((0, 1, 0))
], 'S4R')
fem_set = FemSet('my_set', [elem], 'elset')
fem_sec = FemSection('my_sec', 'shell', fem_set, mat, thickness=0.02)
p = get_fsec_sh_collection()
self.assertFalse(fem_sec in p.fem.sections)
def test_negative_sec_contained(part_with_beam):
# A minor change in section box thickness
sec = Section("myBG", from_str="BG800x400x20x40")
mat = Material("my_mat")
bm = Beam("my_beam", (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], "line")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec",
"line",
fem_set,
mat,
sec,
local_z=(0, 0, 1))
assert fem_sec not in part_with_beam.fem.sections
def test_negative_mat_contained(part_with_beam):
# A minor change in material property (S420 instead of S355)
sec = Section("myBG", from_str="BG800x400x30x40")
mat = Material("my_mat", CarbonSteel("S420"))
bm = Beam("my_beam", (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], "line")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec",
"line",
fem_set,
mat,
sec,
local_z=(0, 0, 1))
assert fem_sec not in part_with_beam.fem.sections
def part_with_shell():
p = Part("my_part")
mat = Material("my_mat")
elem = Elem(
1,
[Node((0, 0, 0)),
Node((1, 0, 0)),
Node((1, 1, 0)),
Node((0, 1, 0))], "quad")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec", "shell", fem_set, mat, thickness=0.01)
for n in elem.nodes:
p.fem.nodes.add(n)
p.fem.elements.add(elem)
p.fem.sets.add(fem_set)
p.fem.sections.add(fem_sec)
return p
def get_fsec_sh_collection():
p = Part('my_part')
mat = Material('my_mat')
elem = Elem(
1,
[Node((0, 0, 0)),
Node((1, 0, 0)),
Node((1, 1, 0)),
Node((0, 1, 0))], 'S4R')
fem_set = FemSet('my_set', [elem], 'elset')
fem_sec = FemSection('my_sec', 'shell', fem_set, mat, thickness=0.01)
for n in elem.nodes:
p.fem.nodes.add(n)
p.fem.elements.add(elem)
p.fem.sets.add(fem_set)
p.fem.sections.add(fem_sec)
return p
def get_mat(match):
d = match.groupdict()
matno = str_to_int(d["matno"])
return Material(
name=mat_names[matno],
mat_id=matno,
mat_model=CarbonSteel(
rho=roundoff(d["rho"]),
E=roundoff(d["young"]),
v=roundoff(d["poiss"]),
alpha=roundoff(d["damp"]),
zeta=roundoff(d["alpha"]),
sig_p=[],
eps_p=[],
sig_y=roundoff(d["yield"]),
),
parent=part,
)
def get_fsec_bm_collection():
sec = Section("myIPE", from_str="BG800x400x30x40")
mat = Material("my_mat")
p = Part("my_part")
bm = Beam("my_beam", (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], "B31")
fem_set = FemSet("my_set", [elem], "elset")
fem_sec = FemSection("my_sec",
"beam",
fem_set,
mat,
sec,
local_z=(0, 0, 1))
p.add_beam(bm)
p.fem.elements.add(elem)
p.fem.sets.add(fem_set)
p.fem.sections.add(fem_sec)
return p
def get_fsec_bm_collection():
sec = Section('myIPE', from_str='BG800x400x30x40')
mat = Material('my_mat')
p = Part('my_part')
bm = Beam('my_beam', (0, 0, 0), (1, 0, 0), sec, mat)
elem = Elem(1, [bm.n1, bm.n2], 'B31')
fem_set = FemSet('my_set', [elem], 'elset')
fem_sec = FemSection('my_sec',
'beam',
fem_set,
mat,
sec,
local_z=(0, 0, 1))
p.add_beam(bm)
p.fem.elements.add(elem)
p.fem.sets.add(fem_set)
p.fem.sections.add(fem_sec)
return p
def beam_ex1(p1=(0, 0, 0), p2=(1.5, 0, 0), profile="IPE400", geom_repr=ElemType.SHELL) -> Assembly:
mat_grade = CarbonSteel.TYPES.S355
bm = Beam("MyBeam", p1, p2, profile, Material("S355", mat_model=CarbonSteel(mat_grade)))
bm.material.model.plasticity_model = DnvGl16Mat(bm.section.t_w, mat_grade)
a = Assembly("Test", user=User("krande")) / [Part("MyPart") / bm]
add_random_cutouts(bm)
# Create a FEM analysis of the beam as a cantilever subjected to gravity loads
p = a.get_part("MyPart")
p.fem = bm.to_fem_obj(0.1, geom_repr)
# Add a set containing ALL elements (necessary for Calculix loads).
fs = p.fem.add_set(FemSet("Eall", [el for el in p.fem.elements], FemSet.TYPES.ELSET))
step = a.fem.add_step(StepImplicit("gravity", nl_geom=True, init_incr=100.0, total_time=100.0))
step.add_load(Load("grav", Load.TYPES.GRAVITY, -9.81 * 800, fem_set=fs))
fix_set = p.fem.add_set(FemSet("bc_nodes", get_beam_end_nodes(bm), FemSet.TYPES.NSET))
a.fem.add_bc(Bc("Fixed", fix_set, [1, 2, 3]))
return a