def setUp(self):
# create materials
steel = Steel()
# create 2d frame analysis object
self.analysis = FrameAnalysis2D()
section1 = Section(area=6e3, ixx=200e6)
section2 = Section(area=4e3, ixx=50e6)
# create nodes
self.node_a = self.analysis.create_node(coords=[0])
self.node_b = self.analysis.create_node(coords=[8000])
self.node_c = self.analysis.create_node(coords=[13000])
# create beam elements
self.element_ab = self.analysis.create_element(
el_type='EB2-2D',
nodes=[self.node_a, self.node_b],
material=steel,
section=section1)
self.element_bc = self.analysis.create_element(
el_type='EB2-2D',
nodes=[self.node_b, self.node_c],
material=steel,
section=section2)
def test_example2_1(self):
nodes = [] # list holding the node objects
elements = [] # list holding the element objects
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create sections
steel = Steel()
section1 = Section(area=6000)
section2 = Section(area=8000)
# create nodes
nodes.append(analysis.create_node(coords=[0, 0]))
nodes.append(analysis.create_node(coords=[6000, 4000]))
nodes.append(analysis.create_node(coords=[9000, 0]))
# create truss elements
elements.append(analysis.create_element(
el_type='Bar2-2D', nodes=[nodes[0], nodes[1]], material=steel, section=section1
))
elements.append(analysis.create_element(
el_type='Bar2-2D', nodes=[nodes[1], nodes[2]], material=steel, section=section2
))
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=nodes[0], val=0, dof=0)
freedom_case.add_nodal_support(node=nodes[0], val=0, dof=1)
freedom_case.add_nodal_support(node=nodes[2], val=0, dof=0)
freedom_case.add_nodal_support(node=nodes[2], val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=nodes[1], val=500e3, dof=0)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
n1_disp = nodes[1].get_displacements(analysis_case)
u = n1_disp[0]
v = n1_disp[1]
self.assertEqual(np.around(u, 2), 2.41)
self.assertEqual(np.around(v, 2), 0.72)
# check axial forces
(_, n1) = elements[0].get_afd(n=1, analysis_case=analysis_case)
(_, n2) = elements[1].get_afd(n=1, analysis_case=analysis_case)
self.assertEqual(np.around(n1/1e3, 1), 400.6)
self.assertEqual(np.around(n2/1e3, 1), -277.8)
def test_example2_3(self):
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create sections
steel = Steel()
section1 = Section(area=4000)
section2 = Section(area=1000)
# create nodes
a = analysis.create_node(coords=[0, 0])
b = analysis.create_node(coords=[2000, 2000])
c = analysis.create_node(coords=[-4000, 2000])
# create truss elements
el1 = analysis.create_element(el_type='Bar2-2D',
nodes=[c, a],
material=steel,
section=section1)
el2 = analysis.create_element(el_type='Bar2-2D',
nodes=[a, b],
material=steel,
section=section2)
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=b, val=0, dof=0)
freedom_case.add_nodal_support(node=b, val=0, dof=1)
freedom_case.add_nodal_support(node=c, val=0, dof=0)
freedom_case.add_nodal_support(node=c, val=0, dof=1)
sup1 = freedom_case.add_nodal_support(node=a, val=0, dof=0)
sup2 = freedom_case.add_nodal_support(node=a, val=-5, dof=1)
# add loads
load_case = cases.LoadCase()
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check reactions
self.assertEqual(np.around(sup1.get_reaction(analysis_case) / 1e3, 1),
181.0)
self.assertEqual(np.around(sup2.get_reaction(analysis_case) / 1e3, 1),
-355.7)
def setUp(self):
steel = Steel()
section = Section()
# create an FrameElement2D elemnetn
self.x = 4
self.y = 3
self.node1 = Node([0, 0])
self.node2 = Node([self.x, self.y])
self.element_frame = FrameElement(
nodes=[self.node1, self.node2], material=steel, section=section,
efs=[True, True, False, False, False, True]
)
self.element_frame2D = FrameElement2D(
nodes=[self.node1, self.node2], material=steel, section=section,
efs=[True, True, False, False, False, False]
)
def preprocessor(length, depth, panels, freq):
w = 10 # load per unit length [N/mm]
dx = length / panels # length of a truss panel
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create materials and sections
steel = Steel()
section_deck = Section(area=3230, ixx=23.6e6) # 200UB25
section_vertical = Section(area=3000, ixx=3.91e6) # 100x9 SHS
section_diagonal = Section(area=314) # 20 dia rod
section_tie = Section(area=1018) # 36 dia rod
# create deck nodes
nodes_deck = []
for i in range(panels + 1):
nodes_deck.append(analysis.create_node(coords=[i * dx]))
# create tie nodes - first node coincides with first deck node
nodes_tie = [nodes_deck[0]]
for i in range(panels - 1):
# fit parabola
x = (i + 1) * dx
y = 4 * depth / length / length * x * x - 4 * depth / length * x
nodes_tie.append(analysis.create_node(coords=[x, y]))
# last node coincides with last deck node
nodes_tie.append(nodes_deck[-1])
# create deck (beam) elements
elements_deck = []
for i in range(panels):
elements_deck.append(
analysis.create_element(el_type='EB2-2D',
nodes=[nodes_deck[i], nodes_deck[i + 1]],
material=steel,
section=section_deck))
# create tie (bar) elements
elements_tie = []
for i in range(panels):
elements_tie.append(
analysis.create_element(el_type='Bar2-2D',
nodes=[nodes_tie[i], nodes_tie[i + 1]],
material=steel,
section=section_tie))
# create vertical (beam) elements
elements_vertical = []
for i in range(panels - 1):
elements_vertical.append(
analysis.create_element(
el_type='EB2-2D',
nodes=[nodes_deck[i + 1], nodes_tie[i + 1]],
material=steel,
section=section_vertical))
# create diagonal (bar) elements
elements_diaongal = []
for i in range(panels - 2):
elements_diaongal.append(
analysis.create_element(
el_type='Bar2-2D',
nodes=[nodes_deck[i + 1], nodes_tie[i + 2]],
material=steel,
section=section_diagonal))
elements_diaongal.append(
analysis.create_element(
el_type='Bar2-2D',
nodes=[nodes_deck[i + 2], nodes_tie[i + 1]],
material=steel,
section=section_diagonal))
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=nodes_deck[0], val=0, dof=0)
freedom_case.add_nodal_support(node=nodes_deck[0], val=0, dof=1)
freedom_case.add_nodal_support(node=nodes_deck[-1], val=0, dof=1)
# add loads
load_case = cases.LoadCase()
# if frequency analysis, don't bother adding load
if not freq:
for el in elements_deck:
load_case.add_element_load(el.generate_udl(q=-w))
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
return (analysis, analysis_case)
def test_fig8(self):
"""Simple Beam – Concentrated Load at Any Point"""
a = self.length * np.random.uniform(0.1, 0.9)
b = self.length - a
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create section
section = Section(ixx=self.ixx)
# create nodes
node_a = analysis.create_node(coords=[0])
node_b = analysis.create_node(coords=[a])
node_c = analysis.create_node(coords=[self.length])
# create beam elements
element_ab = analysis.create_element(el_type='EB2-2D',
nodes=[node_a, node_b],
material=self.steel,
section=section)
element_bc = analysis.create_element(el_type='EB2-2D',
nodes=[node_b, node_c],
material=self.steel,
section=section)
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=node_a, val=0, dof=0)
freedom_case.add_nodal_support(node=node_a, val=0, dof=1)
freedom_case.add_nodal_support(node=node_c, val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=node_b, val=self.pl, dof=1)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check displacements
def analytical_disp_ab(x):
factor = self.pl * b * x / 6 / self.elastic_modulus / self.ixx / self.length
l0 = self.length
return factor * (l0 * l0 - b * b - x * x)
def analytical_disp_bc(x):
l0 = self.length
factor = self.pl * a * (
l0 - x) / 6 / self.elastic_modulus / self.ixx / l0
return factor * (2 * l0 * x - a * a - x * x)
# get displacements
displacements_ab = element_ab.get_displacements(21, analysis_case)
displacements_bc = element_bc.get_displacements(21, analysis_case)
# loop through each station
for disp in displacements_ab:
xi = disp[0]
x = a * xi
v = disp[2]
# check displacements
self.assertTrue(np.isclose(v, analytical_disp_ab(x), atol=1e-06))
# loop through each station
for disp in displacements_bc:
xi = disp[0]
x = b * xi + a
v = disp[2]
# check displacements
self.assertTrue(np.isclose(v, analytical_disp_bc(x), atol=1e-06))
# check max displacement
if a > b:
aa = a
bb = b
disps = displacements_ab
else:
aa = b
bb = a
disps = displacements_bc
l0 = self.length
v_max = (self.pl * aa * bb *
(aa + 2 * bb) * np.sqrt(3 * aa * (aa + 2 * bb))) / (
27 * self.elastic_modulus * self.ixx * l0)
# check value
self.assertTrue(
np.isclose(abs(v_max), max(np.abs(disps[:, 2])), atol=1e-06))
# check position of max displacement
pos = np.sqrt((aa * (aa + 2 * bb)) / 3)
if b > a:
pos = self.length - pos
x = 1 / b * (pos - a)
else:
x = pos / a
self.assertTrue(
np.isclose(x, disps[np.abs(disps[:, 2]).argmax(), 0], atol=1e-06))
# check displacement at point load
v_ab = self.pl * a * a * b * b / 3 / self.elastic_modulus / self.ixx / self.length
self.assertTrue(np.isclose(v_ab, displacements_bc[0, 2], atol=1e-06))
# check bending moments
def analytical_bmd_ab(x):
return self.pl * b * x / self.length
def analytical_bmd_bc(x):
x = self.length - x
return self.pl * a * x / self.length
# get bmd
(xis_ab, bmd_ab) = element_ab.get_bmd(11, analysis_case)
(xis_bc, bmd_bc) = element_bc.get_bmd(11, analysis_case)
# loop through each station
for (i, m) in enumerate(bmd_ab):
xi = xis_ab[i]
x = a * xi
# check bending moment
self.assertTrue(np.isclose(m, analytical_bmd_ab(x), atol=1e-06))
# loop through each station
for (i, m) in enumerate(bmd_bc):
xi = xis_bc[i]
x = a + b * xi
# check bending moment
self.assertTrue(np.isclose(m, analytical_bmd_bc(x), atol=1e-06))
# check max bending moment
m_max = self.pl * a * b / self.length
# check value
self.assertTrue(np.isclose(abs(m_max), max(np.abs(bmd_ab)),
atol=1e-06))
# check position
self.assertTrue(
np.isclose(1, xis_ab[np.abs(bmd_ab).argmax()], atol=1e-06))
# check shear force
def analytical_sfd_ab(x):
return -self.pl * b / self.length
def analytical_sfd_bc(x):
return self.pl * a / self.length
# get sfd
(xis, sfd_ab) = element_ab.get_sfd(11, analysis_case)
(xis, sfd_bc) = element_bc.get_sfd(11, analysis_case)
# loop through each station
for (i, sf) in enumerate(sfd_ab):
xi = xis_ab[i]
x = a * xi
# check shear force
self.assertTrue(np.isclose(sf, analytical_sfd_ab(x), atol=1e-06))
# loop through each station
for (i, sf) in enumerate(sfd_bc):
xi = xis_bc[i]
x = a + b * xi
# check shear force
self.assertTrue(np.isclose(sf, analytical_sfd_bc(x), atol=1e-06))
def test_fig7(self):
"""Simple Beam – Concentrated Load at Center"""
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create section
section = Section(ixx=self.ixx)
# create nodes
node_a = analysis.create_node(coords=[0])
node_b = analysis.create_node(coords=[self.length * 0.5])
node_c = analysis.create_node(coords=[self.length])
# create beam elements
element_ab = analysis.create_element(el_type='EB2-2D',
nodes=[node_a, node_b],
material=self.steel,
section=section)
element_bc = analysis.create_element(el_type='EB2-2D',
nodes=[node_b, node_c],
material=self.steel,
section=section)
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=node_a, val=0, dof=0)
freedom_case.add_nodal_support(node=node_a, val=0, dof=1)
freedom_case.add_nodal_support(node=node_c, val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=node_b, val=self.pl, dof=1)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check displacements
def analytical_disp_ab(x):
factor = self.pl * x / 48 / self.elastic_modulus / self.ixx
l0 = self.length
return factor * (3 * l0 * l0 - 4 * x * x)
def analytical_disp_bc(x):
x = self.length - x
factor = self.pl * x / 48 / self.elastic_modulus / self.ixx
l0 = self.length
return factor * (3 * l0 * l0 - 4 * x * x)
# get displacements
displacements_ab = element_ab.get_displacements(11, analysis_case)
displacements_bc = element_bc.get_displacements(11, analysis_case)
# loop through each station
for disp in displacements_ab:
xi = disp[0]
x = self.length * 0.5 * xi
v = disp[2]
# check displacements
self.assertTrue(np.isclose(v, analytical_disp_ab(x), atol=1e-06))
# loop through each station
for disp in displacements_bc:
xi = disp[0]
x = self.length * 0.5 + self.length * 0.5 * xi
v = disp[2]
# check displacements
self.assertTrue(np.isclose(v, analytical_disp_bc(x), atol=1e-06))
# check max displacement
l0 = self.length
v_max = self.pl * l0 * l0 * l0 / 48 / self.elastic_modulus / self.ixx
# check value
self.assertTrue(
np.isclose(abs(v_max),
max(np.abs(displacements_ab[:, 2])),
atol=1e-06))
# check position
self.assertTrue(
np.isclose(1,
displacements_ab[np.abs(displacements_ab[:,
2]).argmax(),
0],
atol=1e-06))
# check bending moments
def analytical_bmd_ab(x):
return self.pl * x / 2
def analytical_bmd_bc(x):
x = self.length - x
return self.pl * x / 2
# get bmd
(xis_ab, bmd_ab) = element_ab.get_bmd(11, analysis_case)
(xis_bc, bmd_bc) = element_bc.get_bmd(11, analysis_case)
# loop through each station
for (i, m) in enumerate(bmd_ab):
xi = xis_ab[i]
x = self.length * 0.5 * xi
# check bending moment
self.assertTrue(np.isclose(m, analytical_bmd_ab(x), atol=1e-06))
# loop through each station
for (i, m) in enumerate(bmd_bc):
xi = xis_bc[i]
x = self.length * 0.5 + self.length * 0.5 * xi
# check bending moment
self.assertTrue(np.isclose(m, analytical_bmd_bc(x), atol=1e-06))
# check max bending moment
l0 = self.length
m_max = self.pl * l0 / 4
# check value
self.assertTrue(np.isclose(abs(m_max), max(np.abs(bmd_ab)),
atol=1e-06))
# check position
self.assertTrue(
np.isclose(1, xis_ab[np.abs(bmd_ab).argmax()], atol=1e-06))
# check shear force
def analytical_sfd_ab(x):
return -self.pl / 2
def analytical_sfd_bc(x):
return self.pl / 2
# get sfd
(xis, sfd_ab) = element_ab.get_sfd(11, analysis_case)
(xis, sfd_bc) = element_bc.get_sfd(11, analysis_case)
# loop through each station
for (i, sf) in enumerate(sfd_ab):
xi = xis_ab[i]
x = self.length * 0.5 * xi
# check shear force
self.assertTrue(np.isclose(sf, analytical_sfd_ab(x), atol=1e-06))
# loop through each station
for (i, sf) in enumerate(sfd_bc):
xi = xis_bc[i]
x = self.length * 0.5 + self.length * 0.5 * xi
# check shear force
self.assertTrue(np.isclose(sf, analytical_sfd_bc(x), atol=1e-06))
def test_fig4(self):
"""Simple Beam – Uniform Load Partially Distributed at Each End"""
a = self.length * np.random.uniform(0.1, 0.4)
c = self.length * np.random.uniform(0.1, 0.4)
b = self.length - a - c
q2 = -np.random.uniform(1, 10)
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create section
section = Section(ixx=self.ixx)
# create nodes
node_a = analysis.create_node(coords=[0])
node_b = analysis.create_node(coords=[a])
node_c = analysis.create_node(coords=[a + b])
node_d = analysis.create_node(coords=[self.length])
# create beam elements
element_ab = analysis.create_element(el_type='EB2-2D',
nodes=[node_a, node_b],
material=self.steel,
section=section)
element_bc = analysis.create_element(el_type='EB2-2D',
nodes=[node_b, node_c],
material=self.steel,
section=section)
element_cd = analysis.create_element(el_type='EB2-2D',
nodes=[node_c, node_d],
material=self.steel,
section=section)
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=node_a, val=0, dof=0)
sup1 = freedom_case.add_nodal_support(node=node_a, val=0, dof=1)
sup2 = freedom_case.add_nodal_support(node=node_d, val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_element_load(element_ab.generate_udl(q=self.q))
load_case.add_element_load(element_cd.generate_udl(q=q2))
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check reactions
r1 = -sup1.get_reaction(analysis_case)
r1_ana = (self.q * a *
(2 * self.length - a) + q2 * c * c) / (2 * self.length)
r2 = -sup2.get_reaction(analysis_case)
r2_ana = (q2 * c *
(2 * self.length - c) + self.q * a * a) / (2 * self.length)
self.assertTrue(np.isclose(r1, r1_ana, atol=1e-06))
self.assertTrue(np.isclose(r2, r2_ana, atol=1e-06))
# check bending moments
def analytical_bmd_ab(x):
return r1 * x - self.q * 0.5 * x * x
def analytical_bmd_bc(x):
return r1 * x - self.q * a * 0.5 * (2 * x - a)
def analytical_bmd_cd(x):
return r2 * (self.length - x) - q2 * (self.length -
x) * (self.length - x) * 0.5
# get bmds
(xis_ab, bmd_ab) = element_ab.get_bmd(11, analysis_case)
(xis_bc, bmd_bc) = element_bc.get_bmd(11, analysis_case)
(xis_cd, bmd_cd) = element_cd.get_bmd(11, analysis_case)
# element_ab - loop through each station
for (i, m) in enumerate(bmd_ab):
xi = xis_ab[i]
x = a * xi
# check bending moments
self.assertTrue(np.isclose(m, analytical_bmd_ab(x), atol=1e-06))
# element_bc - loop through each station
for (i, m) in enumerate(bmd_bc):
xi = xis_bc[i]
x = b * xi + a
# check bending moments
self.assertTrue(np.isclose(m, analytical_bmd_bc(x), atol=1e-06))
# element_cd - loop through each station
for (i, m) in enumerate(bmd_cd):
xi = xis_cd[i]
x = c * xi + a + b
# check bending moments
self.assertTrue(np.isclose(m, analytical_bmd_cd(x), atol=1e-06))
# check max bending moment
if abs(r1) < abs(self.q * a):
m_max = r1 * r1 / 2 / self.q
pos = r1 / self.q
x = pos / a
# check value
self.assertTrue(
np.isclose(abs(m_max), max(np.abs(bmd_ab)), atol=1e-06))
# check position
self.assertTrue(
np.isclose(x, xis_ab[np.abs(bmd_ab).argmax()], atol=1e-06))
if abs(r2) < abs(q2 * c):
m_max = r2 * r2 / 2 / q2
pos = self.length - r2 / q2
x = 1 / c * (pos - a - b)
# check value
self.assertTrue(
np.isclose(abs(m_max), max(np.abs(bmd_cd)), atol=1e-06))
# check position
self.assertTrue(
np.isclose(x, xis_cd[np.abs(bmd_cd).argmax()], atol=1e-06))
# check shear force
def analytical_sfd_ab(x):
return -r1 + self.q * x
def analytical_sfd_bc(x):
return -r1 + self.q * a
def analytical_sfd_cd(x):
return r2 - q2 * (self.length - x)
# get sfds
(xis_ab, sfd_ab) = element_ab.get_sfd(11, analysis_case)
(xis_bc, sfd_bc) = element_bc.get_sfd(11, analysis_case)
(xis_cd, sfd_cd) = element_cd.get_sfd(11, analysis_case)
# element_ab - loop through each station
for (i, sf) in enumerate(sfd_ab):
xi = xis_ab[i]
x = a * xi
# check shear forces
self.assertTrue(np.isclose(sf, analytical_sfd_ab(x), atol=1e-06))
# element_bc - loop through each station
for (i, sf) in enumerate(sfd_bc):
xi = xis_bc[i]
x = b * xi + a
# check shear forces
self.assertTrue(np.isclose(sf, analytical_sfd_bc(x), atol=1e-06))
# element_cd - loop through each station
for (i, sf) in enumerate(sfd_cd):
xi = xis_cd[i]
x = c * xi + a + b
# check shear forces
self.assertTrue(np.isclose(sf, analytical_sfd_cd(x), atol=1e-06))
def test_fig3(self):
"""Simple Beam – Uniform Load Partially Distributed at One End"""
a = self.length * np.random.uniform(0.1, 0.9)
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create section
section = Section(ixx=self.ixx)
# create nodes
node_a = analysis.create_node(coords=[0])
node_b = analysis.create_node(coords=[a])
node_c = analysis.create_node(coords=[self.length])
# create beam elements
element_ab = analysis.create_element(el_type='EB2-2D',
nodes=[node_a, node_b],
material=self.steel,
section=section)
element_bc = analysis.create_element(el_type='EB2-2D',
nodes=[node_b, node_c],
material=self.steel,
section=section)
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=node_a, val=0, dof=0)
sup1 = freedom_case.add_nodal_support(node=node_a, val=0, dof=1)
sup2 = freedom_case.add_nodal_support(node=node_c, val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_element_load(element_ab.generate_udl(q=self.q))
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check reactions
r1 = -sup1.get_reaction(analysis_case)
r2 = -sup2.get_reaction(analysis_case)
self.assertTrue(
np.isclose(r1,
self.q * a / 2 / self.length * (2 * self.length - a),
atol=1e-06))
self.assertTrue(
np.isclose(r2, self.q * a * a / 2 / self.length, atol=1e-06))
# check displacements
def analytical_disp_ab(x):
l0 = self.length
factor = self.q * x / 24 / self.elastic_modulus / self.ixx / l0
return factor * (a * a * (2 * l0 - a) *
(2 * l0 - a) - 2 * a * x * x *
(2 * l0 - a) + l0 * x * x * x)
def analytical_disp_bc(x):
l0 = self.length
factor = self.q * a * a * (
l0 - x) / 24 / self.elastic_modulus / self.ixx / l0
return factor * (4 * x * l0 - 2 * x * x - a * a)
# get displacements
displacements_ab = element_ab.get_displacements(11, analysis_case)
displacements_bc = element_bc.get_displacements(11, analysis_case)
# loop through each station
for disp in displacements_ab:
xi = disp[0]
x = a * xi
v = disp[2]
# check displacements
self.assertTrue(np.isclose(v, analytical_disp_ab(x), atol=1e-06))
# loop through each station
for disp in displacements_bc:
xi = disp[0]
x = (self.length - a) * xi + a
v = disp[2]
# check displacements
self.assertTrue(np.isclose(v, analytical_disp_bc(x), atol=1e-06))
# check bending moments
def analytical_bmd_ab(x):
return r1 * x - self.q * x * x / 2
def analytical_bmd_bc(x):
return r2 * (self.length - x)
# get bmds
(xis_ab, bmd_ab) = element_ab.get_bmd(11, analysis_case)
(xis_bc, bmd_bc) = element_bc.get_bmd(11, analysis_case)
# element_ab - loop through each station
for (i, m) in enumerate(bmd_ab):
xi = xis_ab[i]
x = a * xi
# check bending moments
self.assertTrue(np.isclose(m, analytical_bmd_ab(x), atol=1e-06))
# element_bc - loop through each station
for (i, m) in enumerate(bmd_bc):
xi = xis_bc[i]
x = (self.length - a) * xi + a
# check bending moments
self.assertTrue(np.isclose(m, analytical_bmd_bc(x), atol=1e-06))
# check max bending moment
m_max = r1 * r1 / 2 / self.q
pos = r1 / self.q
x = pos / a
# check value
self.assertTrue(np.isclose(abs(m_max), max(np.abs(bmd_ab)),
atol=1e-06))
# check position
self.assertTrue(
np.isclose(x, xis_ab[np.abs(bmd_ab).argmax()], atol=1e-06))
# check shear force
def analytical_sfd_ab(x):
return -r1 + self.q * x
def analytical_sfd_bc(x):
return r2
# get sfds
(xis_ab, sfd_ab) = element_ab.get_sfd(11, analysis_case)
(xis_bc, sfd_bc) = element_bc.get_sfd(11, analysis_case)
# element_ab - loop through each station
for (i, sf) in enumerate(sfd_ab):
xi = xis_ab[i]
x = a * xi
# check shear forces
self.assertTrue(np.isclose(sf, analytical_sfd_ab(x), atol=1e-06))
# element_bc - loop through each station
for (i, sf) in enumerate(sfd_bc):
xi = xis_bc[i]
x = (self.length - a) * xi + a
# check shear forces
self.assertTrue(np.isclose(sf, analytical_sfd_bc(x), atol=1e-06))
def test_fig1(self):
"""Simple Beam – Uniformly Distributed Load"""
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create section
section = Section(ixx=self.ixx)
# create nodes
node_a = analysis.create_node(coords=[0])
node_b = analysis.create_node(coords=[self.length])
# create beam elements
element = analysis.create_element(el_type='EB2-2D',
nodes=[node_a, node_b],
material=self.steel,
section=section)
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=node_a, val=0, dof=0)
freedom_case.add_nodal_support(node=node_a, val=0, dof=1)
freedom_case.add_nodal_support(node=node_b, val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_element_load(element.generate_udl(q=self.q))
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check displacements
def analytical_disp(x):
factor = self.q * x / 24 / self.elastic_modulus / self.ixx
l0 = self.length
return factor * (l0 * l0 * l0 - 2 * l0 * x * x + x * x * x)
# get displacements
displacements = element.get_displacements(11, analysis_case)
# loop through each station
for disp in displacements:
xi = disp[0]
x = self.length * xi
v = disp[2]
# check displacements
self.assertTrue(np.isclose(v, analytical_disp(x), atol=1e-06))
# check max displacement
l0 = self.length
v_max = 5 * self.q * l0 * l0 * l0 * l0 / 384 / self.elastic_modulus / self.ixx
# check value
self.assertTrue(
np.isclose(abs(v_max), max(np.abs(displacements[:, 2]))))
# check position
self.assertTrue(
np.isclose(0.5,
displacements[np.abs(displacements[:, 2]).argmax(), 0],
atol=1e-06))
# check bending moments
def analytical_bmd(x):
return self.q * x / 2 * (self.length - x)
# get bmd
(xis, bmd) = element.get_bmd(11, analysis_case)
# loop through each station
for (i, m) in enumerate(bmd):
xi = xis[i]
x = self.length * xi
# check bending moment
self.assertTrue(np.isclose(m, analytical_bmd(x), atol=1e-06))
# check max bending moment
l0 = self.length
m_max = self.q * l0 * l0 / 8
# check value
self.assertTrue(np.isclose(abs(m_max), max(np.abs(bmd)), atol=1e-06))
# check position
self.assertTrue(np.isclose(0.5, xis[np.abs(bmd).argmax()], atol=1e-06))
# check shear force
def analytical_sfd(x):
return self.q * (x - self.length / 2)
# get sfd
(xis, sfd) = element.get_sfd(11, analysis_case)
# loop through each station
for (i, sf) in enumerate(sfd):
xi = xis[i]
x = self.length * xi
# check shear force
self.assertTrue(np.isclose(sf, analytical_sfd(x), atol=1e-06))
def calcPeakDeflection(self, fname, F_r_std, H_fs, E, I, mue, nz, z_lev_fs):
# Setting up dynamic calculation
# ------------
# preprocessor
# ---------
# constants & lists
L = H_fs # length of the beam [m]
n = nz # no of nodes [-]
z = np.append(L, z_lev_fs) # coordinates [m], append top of building
z = np.append(z, 0) # coordinates [m], append support node
num_modes = 1
# everything starts with the analysis object
analysis = FrameAnalysis2D()
# materials and sections are objects
mat_dummy = Material("Dummy", E, 0.3, mue, colour='w')
section = Section(area=1, ixx=I)
# nodes are objects
nodes = []
for i in range(0,n+2): #! n+2 (support, tip)
node = analysis.create_node(coords=[0, z[i]])
nodes.append(node)
# and so are beams!
beams = []
for i in range(0,n+1): #! n+1 (support, tip)
beam = analysis.create_element(
el_type='EB2-2D', nodes=[nodes[i], nodes[i+1]], material=mat_dummy, section=section)
beams.append(beam)
# boundary conditions are objects
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=nodes[-1], val=0, dof=0)
freedom_case.add_nodal_support(node=nodes[-1], val=0, dof=1)
freedom_case.add_nodal_support(node=nodes[-1], val=0, dof=5)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=cases.LoadCase())
# ----------------
# frequency solver
# ----------------
settings = SolverSettings()
settings.natural_frequency.time_info = True
settings.natural_frequency.num_modes = num_modes
solver = NaturalFrequency(
analysis=analysis, analysis_cases=[analysis_case], solver_settings=settings)
# Manual solver, see feastruct/solvers/naturalfrequency.py, in order
# to extract mass/stiffness-matrix and eigenvectors
# assign the global degree of freedom numbers
solver.assign_dofs()
# Get the global stiffness / mass matrix
(K, Kg) = solver.assemble_stiff_matrix()
M = solver.assemble_mass_matrix()
# apply the boundary conditions
K_mod = solver.remove_constrained_dofs(K=K, analysis_case=analysis_case)
M_mod = solver.remove_constrained_dofs(K=M, analysis_case=analysis_case)
# Solve for the eigenvalues
(w, v) = solver.solve_eigenvalue(A=K_mod, M=M_mod, eigen_settings=settings.natural_frequency)
# compute natural frequencies in Hz
f = np.sqrt(w) / 2 / np.pi
# Normalize Eigenvector
v = v / v[0] * L
# # Get only dof ux
# u = np.zeros(n+1)
# for i in range(0, n+1):
# j = i * 3
# u[i] = v[j]
# Get generalized quantities
K_mod = K_mod.toarray()
K_gen = np.dot(np.dot(v.T, K_mod), v)
M_mod = M_mod.toarray()
M_gen = np.dot(np.dot(v.T, M_mod), v)
# To check, compute
# f_k = np.sqrt(K_gen/M_gen) / 2 / np.pi
# print(f/f_k)
# K_gen = 3 * E * I /(L^3) / L
K_gen = K_gen[0][0]
# Calculate peak displacement
delta_r_std = v[0][0] / K_gen * F_r_std
g_peak = response.calcPeakFactor(self, 3600, f[0]) # Peak Factor
delta_r_max = g_peak * delta_r_std
writeToTxt(fname, "delta_r_std: " + '{:02.3f}'.format(delta_r_std))
writeToTxt(fname, "g_peak: " + '{:02.3f}'.format(g_peak))
writeToTxt(fname, "delta_r_max: " + '{:02.3f}'.format(delta_r_max))
def test_example3_2(self):
nodes = [] # list holding the node objects
elements = [] # list holding the element objects
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create sections
steel = Steel()
section1 = Section(area=15e3)
section2 = Section(area=18e3)
section3 = Section(area=20e3)
# create nodes
nodes.append(analysis.create_node(coords=[0, 0]))
nodes.append(
analysis.create_node(coords=[4000 / np.tan(np.pi / 6), 4000]))
nodes.append(
analysis.create_node(coords=[4000 / np.tan(np.pi / 6) + 4000, 0]))
# create truss elements
elements.append(
analysis.create_element(el_type='Bar2-2D',
nodes=[nodes[0], nodes[1]],
material=steel,
section=section1))
elements.append(
analysis.create_element(el_type='Bar2-2D',
nodes=[nodes[1], nodes[2]],
material=steel,
section=section3))
elements.append(
analysis.create_element(el_type='Bar2-2D',
nodes=[nodes[0], nodes[2]],
material=steel,
section=section2))
# add supports
freedom_case = cases.FreedomCase()
sup1 = freedom_case.add_nodal_support(node=nodes[0], val=0, dof=0)
sup2 = freedom_case.add_nodal_support(node=nodes[0], val=0, dof=1)
sup3 = freedom_case.add_nodal_support(node=nodes[2], val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=nodes[1],
val=500e3 * np.cos(2 * np.pi / 9),
dof=0)
load_case.add_nodal_load(node=nodes[1],
val=500e3 * np.sin(2 * np.pi / 9),
dof=1)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
node_a = nodes[1]
node_b = nodes[2]
dofs_a = node_a.get_dofs(node_a.nfs)
dofs_b = node_b.get_dofs(node_b.nfs)
u_a = dofs_a[0].get_displacement(analysis_case)
v_a = dofs_a[1].get_displacement(analysis_case)
u_b = dofs_b[0].get_displacement(analysis_case)
self.assertEqual(np.around(u_a, 2), 0.87)
self.assertEqual(np.around(v_a, 2), 1.24)
self.assertEqual(np.around(u_b, 2), -0.19)
# check axial forces
n1 = elements[0].get_afd(n=1, analysis_case=analysis_case)
n2 = elements[1].get_afd(n=1, analysis_case=analysis_case)
n3 = elements[2].get_afd(n=1, analysis_case=analysis_case)
self.assertEqual(np.around(n1 / 1e3, 1), 515.7)
self.assertEqual(np.around(n2 / 1e3, 1), 89.9)
self.assertEqual(np.around(n3 / 1e3, 1), -63.6)
# check reactions
rc_x = sup1.get_reaction(analysis_case=analysis_case)
rc_y = sup2.get_reaction(analysis_case=analysis_case)
rb_y = sup3.get_reaction(analysis_case=analysis_case)
self.assertEqual(np.around(rc_x / 1e3, 1), -383.0)
self.assertEqual(np.around(rc_y / 1e3, 1), -257.8)
self.assertEqual(np.around(rb_y / 1e3, 1), -63.6)
def test_example2_2(self):
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create sections
steel = Steel()
section1 = Section(area=5000)
section2 = Section(area=3000)
# create nodes
a = analysis.create_node(coords=[0, 0])
b = analysis.create_node(coords=[3000, 3000])
c = analysis.create_node(coords=[3000, -3000])
d = analysis.create_node(coords=[-3000 / np.tan(np.pi / 6), 3000])
e = analysis.create_node(coords=[-3000 / np.tan(np.pi / 6), -3000])
# create truss elements
el1 = analysis.create_element(el_type='Bar2-2D',
nodes=[e, a],
material=steel,
section=section1)
el2 = analysis.create_element(el_type='Bar2-2D',
nodes=[d, a],
material=steel,
section=section1)
el3 = analysis.create_element(el_type='Bar2-2D',
nodes=[b, a],
material=steel,
section=section2)
el4 = analysis.create_element(el_type='Bar2-2D',
nodes=[c, a],
material=steel,
section=section2)
# add supports
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=b, val=0, dof=0)
freedom_case.add_nodal_support(node=b, val=0, dof=1)
freedom_case.add_nodal_support(node=c, val=0, dof=0)
freedom_case.add_nodal_support(node=c, val=0, dof=1)
freedom_case.add_nodal_support(node=d, val=0, dof=0)
freedom_case.add_nodal_support(node=d, val=0, dof=1)
freedom_case.add_nodal_support(node=e, val=0, dof=0)
freedom_case.add_nodal_support(node=e, val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=a, val=1000e3, dof=0)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case,
load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
dofs = a.get_dofs(a.nfs)
u = dofs[0].get_displacement(analysis_case)
v = dofs[1].get_displacement(analysis_case)
self.assertEqual(np.around(u, 2), 2.55)
self.assertEqual(np.around(v, 2), 0)
# check axial forces
n1 = el1.get_afd(n=1, analysis_case=analysis_case)
n2 = el2.get_afd(n=1, analysis_case=analysis_case)
n3 = el3.get_afd(n=1, analysis_case=analysis_case)
n4 = el4.get_afd(n=1, analysis_case=analysis_case)
self.assertEqual(np.around(n1 / 1e3, 1), 368.8)
self.assertEqual(np.around(n2 / 1e3, 1), 368.8)
self.assertEqual(np.around(n3 / 1e3, 1), -255.5)
self.assertEqual(np.around(n4 / 1e3, 1), -255.5)
def test_example5_7(self):
l_a = np.sqrt(8000 * 8000 - 3000 * 3000)
# create materials
steel = Steel()
# create 2d frame analysis object
analysis = FrameAnalysis2D()
section = Section(area=6e3, ixx=200e6)
# create nodes
node_a = analysis.create_node(coords=[0])
node_b = analysis.create_node(coords=[l_a, 3000])
node_c = analysis.create_node(coords=[l_a + 8000, 3000])
# create beam elements
element_ab = analysis.create_element(
el_type='EB2-2D', nodes=[node_a, node_b], material=steel, section=section
)
element_bc = analysis.create_element(
el_type='EB2-2D', nodes=[node_b, node_c], material=steel, section=section
)
# add supports
freedom_case = cases.FreedomCase()
sup_a = [0, 0, 0]
sup_a[0] = freedom_case.add_nodal_support(node=node_a, val=0, dof=0)
sup_a[1] = freedom_case.add_nodal_support(node=node_a, val=0, dof=1)
sup_a[2] = freedom_case.add_nodal_support(node=node_a, val=0, dof=5)
sup_c = [0, 0, 0]
sup_c[0] = freedom_case.add_nodal_support(node=node_c, val=0, dof=0)
sup_c[1] = freedom_case.add_nodal_support(node=node_c, val=0, dof=1)
sup_c[2] = freedom_case.add_nodal_support(node=node_c, val=0, dof=5)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=node_b, val=50e3 * 3000 / 8000, dof=0)
load_case.add_nodal_load(node=node_b, val=-50e3 * l_a / 8000, dof=1)
load_case.add_element_load(element_bc.generate_udl(q=-4))
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
disp_b = node_b.get_displacements(analysis_case)
u_b = disp_b[0]
v_b = disp_b[1]
r_b = disp_b[5]
self.assertEqual(np.around(u_b, 4), 0.9950)
self.assertEqual(np.around(v_b, 3), -4.982)
self.assertEqual(np.around(r_b, 6), -0.000534)
# check reactions
ra_x = sup_a[0].get_reaction(analysis_case=analysis_case)
ra_y = sup_a[1].get_reaction(analysis_case=analysis_case)
ra_m = sup_a[2].get_reaction(analysis_case=analysis_case)
rc_x = sup_c[0].get_reaction(analysis_case=analysis_case)
rc_y = sup_c[1].get_reaction(analysis_case=analysis_case)
rc_m = sup_c[2].get_reaction(analysis_case=analysis_case)
self.assertEqual(np.around(ra_x/1e3, 1), 130.5)
self.assertEqual(np.around(ra_y/1e3, 1), 55.7)
self.assertEqual(np.around(ra_m/1e6, 2), 13.37)
self.assertEqual(np.around(rc_x/1e3, 1), -149.3)
self.assertEqual(np.around(rc_y/1e3, 1), 22.7)
self.assertEqual(np.around(rc_m/1e6, 2), -45.36)
def test_example5_4(self):
# create materials
steel = Steel()
# create 3d frame analysis object
analysis = FrameAnalysis3D()
section_ab = Section(area=20e3)
section_ac = Section(area=30e3)
section_ad = Section(area=40e3)
section_ae = Section(area=30e3)
# create nodes
node_a = analysis.create_node(coords=[2000, 4000, 8000])
node_b = analysis.create_node(coords=[0, 0, 0])
node_c = analysis.create_node(coords=[8000, 0, 0])
node_d = analysis.create_node(coords=[8000, 6000, 0])
node_e = analysis.create_node(coords=[0, 6000, 0])
# create truss elements
element_ab = analysis.create_element(
el_type='Bar2-3D', nodes=[node_a, node_b], material=steel, section=section_ab
)
element_ac = analysis.create_element(
el_type='Bar2-3D', nodes=[node_a, node_c], material=steel, section=section_ac
)
element_ad = analysis.create_element(
el_type='Bar2-3D', nodes=[node_a, node_d], material=steel, section=section_ad
)
element_ae = analysis.create_element(
el_type='Bar2-3D', nodes=[node_a, node_e], material=steel, section=section_ae
)
# add supports
freedom_case = cases.FreedomCase()
sup_b = [0, 0, 0]
sup_c = [0, 0, 0]
sup_d = [0, 0, 0]
sup_e = [0, 0, 0]
sup_b[0] = freedom_case.add_nodal_support(node=node_b, val=0, dof=0)
sup_b[1] = freedom_case.add_nodal_support(node=node_b, val=0, dof=1)
sup_b[2] = freedom_case.add_nodal_support(node=node_b, val=0, dof=2)
sup_c[0] = freedom_case.add_nodal_support(node=node_c, val=0, dof=0)
sup_c[1] = freedom_case.add_nodal_support(node=node_c, val=0, dof=1)
sup_c[2] = freedom_case.add_nodal_support(node=node_c, val=0, dof=2)
sup_d[0] = freedom_case.add_nodal_support(node=node_d, val=0, dof=0)
sup_d[1] = freedom_case.add_nodal_support(node=node_d, val=0, dof=1)
sup_d[2] = freedom_case.add_nodal_support(node=node_d, val=0, dof=2)
sup_e[0] = freedom_case.add_nodal_support(node=node_e, val=0, dof=0)
sup_e[1] = freedom_case.add_nodal_support(node=node_e, val=0, dof=1)
sup_e[2] = freedom_case.add_nodal_support(node=node_e, val=0, dof=2)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=node_a, val=200e3, dof=0)
load_case.add_nodal_load(node=node_a, val=600e3, dof=1)
load_case.add_nodal_load(node=node_a, val=-800e3, dof=2)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
disp_a = node_a.get_displacements(analysis_case)
u_a = disp_a[0]
v_a = disp_a[1]
w_a = disp_a[2]
self.assertEqual(np.around(u_a, 3), 0.178)
self.assertEqual(np.around(v_a, 3), 2.722)
self.assertEqual(np.around(w_a, 3), -0.487)
# check reactions
rb_x = sup_b[0].get_reaction(analysis_case=analysis_case)
rb_y = sup_b[1].get_reaction(analysis_case=analysis_case)
rb_z = sup_b[2].get_reaction(analysis_case=analysis_case)
rc_x = sup_c[0].get_reaction(analysis_case=analysis_case)
rc_y = sup_c[1].get_reaction(analysis_case=analysis_case)
rc_z = sup_c[2].get_reaction(analysis_case=analysis_case)
rd_x = sup_d[0].get_reaction(analysis_case=analysis_case)
rd_y = sup_d[1].get_reaction(analysis_case=analysis_case)
rd_z = sup_d[2].get_reaction(analysis_case=analysis_case)
re_x = sup_e[0].get_reaction(analysis_case=analysis_case)
re_y = sup_e[1].get_reaction(analysis_case=analysis_case)
re_z = sup_e[2].get_reaction(analysis_case=analysis_case)
self.assertEqual(np.around(rb_x/1e3, 1), -76.4)
self.assertEqual(np.around(rb_y/1e3, 1), -152.8)
self.assertEqual(np.around(rb_z/1e3, 1), -305.6)
self.assertEqual(np.around(rc_x/1e3, 1), 170.8)
self.assertEqual(np.around(rc_y/1e3, 1), -113.9)
self.assertEqual(np.around(rc_z/1e3, 1), -227.8)
self.assertEqual(np.around(rd_x/1e3, 1), -470.8)
self.assertEqual(np.around(rd_y/1e3, 1), -156.9)
self.assertEqual(np.around(rd_z/1e3, 1), 627.8)
self.assertEqual(np.around(re_x/1e3, 1), 176.4)
self.assertEqual(np.around(re_y/1e3, 1), -176.4)
self.assertEqual(np.around(re_z/1e3, 1), 705.6)
def test_example5_6(self):
# create materials
steel = Steel()
# create 2d frame analysis object
analysis = FrameAnalysis2D()
section_ab = Section(area=6e3, ixx=200e6)
section_bc = Section(area=4e3, ixx=50e6)
# create nodes
node_a = analysis.create_node(coords=[0])
node_b = analysis.create_node(coords=[8000])
node_p = analysis.create_node(coords=[10000])
node_c = analysis.create_node(coords=[13000])
# create beam elements
element_ab = analysis.create_element(
el_type='EB2-2D', nodes=[node_a, node_b], material=steel, section=section_ab
)
element_bp = analysis.create_element(
el_type='EB2-2D', nodes=[node_b, node_p], material=steel, section=section_bc
)
element_pc = analysis.create_element(
el_type='EB2-2D', nodes=[node_p, node_c], material=steel, section=section_bc
)
# add supports
freedom_case = cases.FreedomCase()
sup_a = freedom_case.add_nodal_support(node=node_a, val=0, dof=1)
sup_b = freedom_case.add_nodal_support(node=node_b, val=0, dof=1)
sup_c = [0, 0, 0]
sup_c[0] = freedom_case.add_nodal_support(node=node_c, val=0, dof=0)
sup_c[1] = freedom_case.add_nodal_support(node=node_c, val=0, dof=1)
sup_c[2] = freedom_case.add_nodal_support(node=node_c, val=0, dof=5)
# add loads
load_case = cases.LoadCase()
load_case.add_element_load(element_ab.generate_udl(q=-2))
load_case.add_nodal_load(node=node_p, val=-20e3, dof=1)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
disp_a = node_a.get_displacements(analysis_case)
disp_b = node_b.get_displacements(analysis_case)
r_a = disp_a[5]
r_b = disp_b[5]
self.assertEqual(np.around(r_a, 7), -5.681e-4)
self.assertEqual(np.around(r_b, 7), 0.696e-4)
# check reactions
ra_y = sup_a.get_reaction(analysis_case=analysis_case)
rb_y = sup_b.get_reaction(analysis_case=analysis_case)
rc_y = sup_c[1].get_reaction(analysis_case=analysis_case)
rc_m = sup_c[2].get_reaction(analysis_case=analysis_case)
self.assertEqual(np.around(ra_y/1e3, 2), 6.13)
self.assertEqual(np.around(rb_y/1e3, 2), 23.00)
self.assertEqual(np.around(rc_y/1e3, 2), 6.87)
self.assertEqual(np.around(rc_m/1e6, 2), -9.32)
def test_example3_3(self):
nodes = [] # list holding the node objects
elements = [] # list holding the element objects
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create sections
steel = Steel()
section1 = Section(area=15e3)
section2 = Section(area=18e3)
section3 = Section(area=20e3)
# create nodes
nodes.append(analysis.create_node(coords=[0, 0]))
nodes.append(analysis.create_node(coords=[4000/np.tan(np.pi/6), 4000]))
nodes.append(analysis.create_node(coords=[4000/np.tan(np.pi/6) + 4000, 0]))
nodes.append(analysis.create_node(coords=[0, 4000]))
# create truss elements
elements.append(analysis.create_element(
el_type='Bar2-2D', nodes=[nodes[0], nodes[1]], material=steel, section=section1
))
elements.append(analysis.create_element(
el_type='Bar2-2D', nodes=[nodes[1], nodes[2]], material=steel, section=section3
))
elements.append(analysis.create_element(
el_type='Bar2-2D', nodes=[nodes[0], nodes[2]], material=steel, section=section2
))
elements.append(analysis.create_element(
el_type='Bar2-2D', nodes=[nodes[3], nodes[1]], material=steel, section=section3
))
# add supports
freedom_case = cases.FreedomCase()
sup1 = freedom_case.add_nodal_support(node=nodes[0], val=0, dof=0)
sup2 = freedom_case.add_nodal_support(node=nodes[0], val=0, dof=1)
sup3 = freedom_case.add_nodal_support(node=nodes[2], val=0, dof=1)
sup4 = freedom_case.add_nodal_support(node=nodes[3], val=0, dof=0)
sup5 = freedom_case.add_nodal_support(node=nodes[3], val=0, dof=1)
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=nodes[1], val=500e3*np.cos(2*np.pi/9), dof=0)
load_case.add_nodal_load(node=nodes[1], val=500e3*np.sin(2*np.pi/9), dof=1)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
disp_a = nodes[1].get_displacements(analysis_case)
disp_b = nodes[2].get_displacements(analysis_case)
u_a = disp_a[0]
v_a = disp_a[1]
u_b = disp_b[0]
self.assertEqual(np.around(u_a, 2), 0.38)
self.assertEqual(np.around(v_a, 2), 1.23)
self.assertEqual(np.around(u_b, 2), -0.44)
# check reactions
rc_x = sup1.get_reaction(analysis_case=analysis_case)
rc_y = sup2.get_reaction(analysis_case=analysis_case)
rb_y = sup3.get_reaction(analysis_case=analysis_case)
rd_x = sup4.get_reaction(analysis_case=analysis_case)
rd_y = sup5.get_reaction(analysis_case=analysis_case)
self.assertEqual(np.around(rc_x/1e3, 1), -162.5)
self.assertEqual(np.around(rc_y/1e3, 1), -177.1)
self.assertEqual(np.around(rb_y/1e3, 1), -144.3)
self.assertEqual(np.around(rd_x/1e3, 1), -220.5)
self.assertEqual(np.around(rd_y/1e3, 1), 0)
# preprocessor
# ------------
# constants & lists
height = 20000 # length of the beam
num_nodes = 21 # number of nodes to use
num_modes = 6 # number of modes to calculate
nodes = [] # list holding the node objects
elements = [] # list holding the element objects
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create materials and sections
steel = Steel()
section = Section(area=10400, ixx=88.3e6)
# create nodes
for i in range(num_nodes):
nodes.append(analysis.create_node(coords=[0, height / (num_nodes - 1) *
i]))
# create beam elements
for i in range(num_nodes - 1):
elements.append(
analysis.create_element(el_type='EB2-2D',
nodes=[nodes[i], nodes[i + 1]],
material=steel,
section=section))
# add supports - fixed base
def __init__(self, buildProp, stiff_red = 0):
"""Inits the class, setting up calculation model
:param buildProp: full scale properties of the building
:type buildProp: :class:`~modelProp.buildProp`
"""
# Setting up calculation model
# ------------
# preprocessor
# ---------
# constants & lists
self.L = buildProp.H # length of the beam [m]
self.n = buildProp.nz # no of nodes [-]
self.z = buildProp.z_lev # coordinates [m]
# everything starts with the analysis object
self.analysis = FrameAnalysis2D()
### NODES
# -------------
# Coordinates for geometrie
self.node_coords_geom = []
for i in range(buildProp.nF+1):
node = i * buildProp.hL
self.node_coords_geom.append(node)
# Sort from bottom to top of building,
# must be done for inserting loads at right order!
self.node_coords_geom = sorted(self.node_coords_geom, reverse=True)
self.node_coords_load = []
for i in range(buildProp.nz):
node = round(buildProp.z_lev[i], 1)
self.node_coords_load.append(node)
# Sort from bottom to top of building,
# must be done for inserting loads at right order!
self.node_coords_load = sorted(self.node_coords_load, reverse=True)
# Merge / sort / remove duplicate nodes
self.node_coords = sorted(list(set(self.node_coords_geom + self.node_coords_load)), reverse=True)
# Insert nodes
self.nodes = []
for i in range(len(self.node_coords)):
node = self.analysis.create_node(coords=[0, self.node_coords[i]])
self.nodes.append(node)
## BEAMS
# -------------
self.beams = []
# Counter for stiffness reduction
j = -1
# Determine coords. where reductions shall be made
hModule = buildProp.H / buildProp.nM
# Reset wall mass to 0
buildProp.M_DL_CWall = 0
buildProp.recalcBuildMass()
# Remark: Reverse node order here, going from bottom to tip
for i in range(1, len(self.nodes)): #! n+1 (support, tip)
# Get z-coord of current node
z_i = self.nodes[-i].y
# Raise counter if next module for reduction is reached
if z_i % hModule == 0:
j = j + 1
# Recalculate dist. mass
# For concrete walls: mue_walls = A_walls [m2] * 2.5 [t/m3]
if buildProp.structSys == 'concreteCore':
mue_DL_CWall= ((buildProp.bCore + buildProp.t)**2 - (buildProp.bCore - buildProp.t)**2) * 2.5
mue_SLS_Tot = buildProp.M_SLS_Tot / buildProp.H + (1 - stiff_red) ** j * mue_DL_CWall
# Add mass of walls to total mass
buildProp.M_DL_CWall += (1 - stiff_red) ** j * mue_DL_CWall * (self.nodes[-i-1].y - self.nodes[-i].y)
else:
raise('No structural system specified')
## MATERIAL
# -------------
self.material = Material("Dummy", buildProp.E, 0.3, mue_SLS_Tot, colour='w')
## SECTION
# -------------
if buildProp.structSys == 'concreteCore':
I = buildProp.I * (1 - stiff_red) ** j
else:
raise('No structural system specified')
self.section = Section(area=1, ixx=I)
# Add beams
beam = self.analysis.create_element(
el_type='EB2-2D', nodes=[self.nodes[-i], self.nodes[-i-1]], material=self.material, section=self.section)
self.beams.append(beam)
# Print stiffness distribution for control
# print('at z = ' + str(self.nodes[-i].y))
# print('I = ' + str(beam.section.ixx))
# Recalculate the building mass, now with walls
buildProp.recalcBuildMass()
# boundary conditions are objects
self.freedom_case = cases.FreedomCase()
self.freedom_case.add_nodal_support(node=self.nodes[-1], val=0, dof=0)
self.freedom_case.add_nodal_support(node=self.nodes[-1], val=0, dof=1)
self.freedom_case.add_nodal_support(node=self.nodes[-1], val=0, dof=5)
def test_example4_15(self):
# create materials
steel = Material(name='steel_imperial', elastic_modulus=29e3, poissons_ratio=0.3, rho=0)
# create 2d frame analysis object
analysis = FrameAnalysis2D()
analysis.post.n_subdiv = 3
beam = Section(ixx=128.5)
# create nodes
n = 20 # number of beam segments (must be an even number to ensure point load in centre)
L = 300 # length
k_L = 15 # spring length
k = 1.5 # foundation modulus
dx = L/n
spring = Section(area=k*dx*k_L/29e3)
beam_nodes = []
spring_nodes = []
# beam nodes
for i in range(n+1):
beam_nodes.append(analysis.create_node(coords=[i*L/n]))
# spring nodes
for i in range(n-1):
spring_nodes.append(analysis.create_node(coords=[(i+1)*L/n, -k_L]))
# create elements
beam_elements = []
spring_elements = []
# create beam elements
for i in range(n):
beam_elements.append(analysis.create_element(
el_type='EB2-2D', nodes=[beam_nodes[i], beam_nodes[i+1]], material=steel,
section=beam
))
# create spring elements
for i in range(n-1):
spring_elements.append(analysis.create_element(
el_type='Bar2-2D', nodes=[beam_nodes[i+1], spring_nodes[i]], material=steel,
section=spring
))
# add supports
freedom_case = cases.FreedomCase()
spring_supports_x = []
spring_supports_y = []
# add end supports
freedom_case.add_nodal_support(node=beam_nodes[0], val=0, dof=0)
freedom_case.add_nodal_support(node=beam_nodes[0], val=0, dof=1)
freedom_case.add_nodal_support(node=beam_nodes[-1], val=0, dof=1)
# add spring support
for spring_node in spring_nodes:
spring_supports_x.append(freedom_case.add_nodal_support(
node=spring_node, val=0, dof=0))
spring_supports_y.append(freedom_case.add_nodal_support(
node=spring_node, val=0, dof=1))
# add loads
load_case = cases.LoadCase()
load_case.add_nodal_load(node=beam_nodes[int(n/2)], val=-40, dof=1)
# add analysis case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=load_case)
# linear static solver
LinearStatic(analysis=analysis, analysis_cases=[analysis_case]).solve()
# check node displacement
disp = beam_nodes[int(n/2)].get_displacements(analysis_case)
v_p = disp[1]
self.assertEqual(np.around(v_p, 3), -0.238)
# check bending moments
(_, m) = beam_elements[int(n/2)].get_bmd(n=2, analysis_case=analysis_case)
self.assertEqual(np.around(m[0], 0), -547)
def calcMeanDeflection(self, fname, F_p_j, H_fs, E, I, nz, z_lev_fs):
# Setting up static calculation
# ------------
# preprocessor
# ---------
# constants & lists
L = H_fs # length of the beam [m]
n = nz # no of nodes [-]
z = np.append(L, z_lev_fs) # coordinates [m], append top of building
z = np.append(z, 0) # coordinates [m], append support node
# everything starts with the analysis object
analysis = FrameAnalysis2D()
# materials and sections are objects
mat_dummy = Material("Dummy", E, 0.3, 1, colour='w')
section = Section(area=1, ixx=I)
# nodes are objects
nodes = []
for i in range(0,n+2): #! n+2 (support, tip)
node = analysis.create_node(coords=[0, z[i]])
nodes.append(node)
# and so are beams!
beams = []
for i in range(0,n+1): #! n+1 (support, tip)
beam = analysis.create_element(
el_type='EB2-2D', nodes=[nodes[i], nodes[i+1]], material=mat_dummy, section=section)
beams.append(beam)
# boundary conditions are objects
freedom_case = cases.FreedomCase()
freedom_case.add_nodal_support(node=nodes[-1], val=0, dof=0)
freedom_case.add_nodal_support(node=nodes[-1], val=0, dof=1)
freedom_case.add_nodal_support(node=nodes[-1], val=0, dof=5)
# so are loads!
load_case = cases.LoadCase()
for i in range(n):
F_p = np.mean(F_p_j[i]) #[in KN]
load_case.add_nodal_load(node=nodes[i+1], val=F_p , dof=0) # i+1 (support, tip)
# an analysis case relates a support case to a load case
analysis_case = cases.AnalysisCase(freedom_case=freedom_case, load_case=load_case)
# ------
# solver
# ------
# you can easily change the solver settings
settings = SolverSettings()
settings.linear_static.time_info = False
# the linear static solver is an object and acts on the analysis object
solver = LinearStatic(analysis=analysis, analysis_cases=[analysis_case], solver_settings=settings)
solver.solve()
# ----
# post
# ----
# there are plenty of post processing options!
# analysis.post.plot_geom(analysis_case=analysis_case)
# analysis.post.plot_geom(analysis_case=analysis_case, deformed=True, def_scale=1e2)
# analysis.post.plot_frame_forces(analysis_case=analysis_case, shear=True)
# analysis.post.plot_frame_forces(analysis_case=analysis_case, moment=True)
# analysis.post.plot_reactions(analysis_case=analysis_case)
# Support reactions, to check bending moment for validation
for support in analysis_case.freedom_case.items:
if support.dof in [5]:
reaction = support.get_reaction(analysis_case=analysis_case)
# read out deformation at top
self.delta_p_mean = nodes[0].get_displacements(analysis_case)[0]
writeToTxt(fname, "delta_p_mean: " + '{:02.3f}'.format(self.delta_p_mean))
# preprocessor
# ------------
# lists
nodes = [] # list holding the node objects
elements = [] # list holding the element objects
freedom_cases = [] # list holding the freedom cases
load_cases = [] # list holding the load cases
analysis_cases = [] # list holding the analysis cases
# create 2d frame analysis object
analysis = FrameAnalysis2D()
# create materials and sections
steel = Steel()
section = Section(area=3230, ixx=23.6e6)
# create nodes
nodes.append(analysis.create_node(coords=[0, 0]))
nodes.append(analysis.create_node(coords=[1500, 0]))
nodes.append(analysis.create_node(coords=[3000, 1500]))
# create beam elements
for i in range(2):
elements.append(
analysis.create_element(el_type='EB2-2D',
nodes=[nodes[i], nodes[i + 1]],
material=steel,
section=section))
# create 3 freedom cases
# preprocessor
# ------------
# constants & lists
L = 5000 # length of the beams
n_el = 12 # number of subdivisions for each beam
nodes = [] # list holding the node objects
elements = [] # list holding the element objects
# create 2d frame analysis object
analysis = FrameAnalysis2D()
analysis.post.n_subdiv = 5
# create materials and sections
steel = Steel()
section = Section(area=1000, ixx=8.333e5)
# create nodes (portal frame)
for i in range(n_el + 1):
nodes.append(analysis.create_node(coords=[0, i * L / n_el]))
for i in range(n_el + 1, 2 * n_el + 1):
nodes.append(analysis.create_node(coords=[(i - n_el) * L / n_el, L]))
for i in range(2 * n_el + 1, 3 * n_el + 1):
nodes.append(
analysis.create_node(coords=[L, L - (i - 2 * n_el) * L / n_el]))
# create elements
for i in range(3 * n_el):
elements.append(