def volume_force_quads(nodes,
elements,
thickness,
freedom,
force_function,
gauss_order=3):
from quadrature import legendre_quad
from shape_functions import iso_quad
from numpy import sum
dimension = len(nodes) * freedom
force = zeros(dimension)
element_nodes = 4
(xi, eta, w) = legendre_quad(gauss_order)
directions_number = len(nodes[0])
for element in elements:
fe = zeros([element_nodes, freedom])
vertices = nodes[element[:], :]
node = zeros([element_nodes, directions_number])
for i in range(len(w)):
(jacobian, shape, shape_dx,
shape_dy) = iso_quad(vertices, xi[i], eta[i])
for j in range(directions_number):
node[:, j] = sum(shape * vertices[:, j])
node[:, j] = sum(shape * vertices[:, j])
for j in range(element_nodes):
fe[j, :] = fe[j, :] + shape[j] * force_function(
node) * thickness * w[i] * jacobian
for i in range(element_nodes):
for j in range(freedom):
force[element[i] * freedom + j] += fe[i, j]
return force
def assembly_quads_stress_strain(nodes,
elements,
thickness,
elasticity_matrix,
gauss_order=2):
# type: (array, array, array, int) -> lil_matrix
"""
Assembly Routine for the Plane Stress-Strain State Analysis using a Mesh of Quadrilaterals
:param nodes: A two-dimensional array of coordinates (nodes)
:param elements: A two-dimensional array of quads (a mesh)
:param thickness: A thickness of an object
:param elasticity_matrix: A two-dimensional array that represents stress-strain relations
:param gauss_order: An order of gaussian quadratures (a count of points used to approximate in each direction)
:return: A global stiffness matrix stored in the CSR sparse format
Order: u_0, v0, u_1, v_1, ..., u_(n-1), v_(n-1); n is nodes count
"""
from quadrature import legendre_quad
from shape_functions import iso_quad
print "The assembly routine is started."
freedom = 2
element_nodes = 4
nodes_count = len(nodes)
dimension = freedom * nodes_count
element_dimension = freedom * element_nodes
global_matrix = lil_matrix((dimension, dimension))
elements_count = len(elements)
(xi, eta, w) = legendre_quad(gauss_order)
for element_index in range(elements_count):
local = zeros((element_dimension, element_dimension))
element = nodes[elements[element_index, :], :]
for i in range(len(w)):
(jacobian, shape, shape_dx,
shape_dy) = iso_quad(element, xi[i], eta[i])
b = array([[
shape_dx[0], 0.0, shape_dx[1], 0.0, shape_dx[2], 0.0,
shape_dx[3], 0.0
],
[
0.0, shape_dy[0], 0.0, shape_dy[1], 0.0,
shape_dy[2], 0.0, shape_dy[3]
],
[
shape_dy[0], shape_dx[0], shape_dy[1], shape_dx[1],
shape_dy[2], shape_dx[2], shape_dy[3], shape_dx[3]
]])
bt = b.conj().transpose()
local = local + thickness * bt.dot(elasticity_matrix).dot(
b) * jacobian * w[i]
for i in range(element_dimension):
ii = elements[element_index, i / freedom] * freedom + i % freedom
for j in range(i, element_dimension):
jj = elements[element_index,
j / freedom] * freedom + j % freedom
global_matrix[ii, jj] += local[i, j]
if i != j:
global_matrix[jj, ii] = global_matrix[ii, jj]
print_progress(element_index, elements_count - 1)
print "\nThe assembly routine is completed."
return global_matrix.tocsr()
def thermal_force_plate_5(nodes,
elements,
thicknesses,
elasticity_matrices,
alpha_t,
gauss_order=3):
from quadrature import legendre_quad
from shape_functions import iso_quad
from numpy import sum, array
freedom = 5
dimension = len(nodes) * freedom
force = zeros(dimension)
element_nodes = 4
(xi, eta, w) = legendre_quad(gauss_order)
alpha = array([alpha_t, alpha_t, 0.0])
h = sum(thicknesses)
for element in elements:
fe = zeros(element_nodes * freedom)
vertices = nodes[element[:], :]
for i in range(len(w)):
(jacobian, shape, shape_dx,
shape_dy) = iso_quad(vertices, xi[i], eta[i])
bm = array([[
shape_dx[0], 0.0, 0.0, 0.0, 0.0, shape_dx[1], 0.0, 0.0, 0.0,
0.0, shape_dx[2], 0.0, 0.0, 0.0, 0.0, shape_dx[3], 0.0, 0.0,
0.0, 0.0
],
[
0.0, shape_dy[0], 0.0, 0.0, 0.0, 0.0, shape_dy[1],
0.0, 0.0, 0.0, 0.0, shape_dy[2], 0.0, 0.0, 0.0,
0.0, shape_dy[3], 0.0, 0.0, 0.0
],
[
shape_dy[0], shape_dx[0], 0.0, 0.0, 0.0,
shape_dy[1], shape_dx[1], 0.0, 0.0, 0.0,
shape_dy[2], shape_dx[2], 0.0, 0.0, 0.0,
shape_dy[3], shape_dx[3], 0.0, 0.0, 0.0
]])
z0 = -h / 2.0
for j in range(len(thicknesses)):
z1 = z0 + thicknesses[j]
df = elasticity_matrices[j]
fe = fe + (z1 - z0) * bm.transpose().dot(df).dot(
alpha) * w[i] * jacobian
z0 = z1
for i in range(element_nodes * freedom):
ii = element[i / freedom] * freedom + i % freedom
force[ii] += fe[i]
return force
def thermal_force_quads(nodes,
elements,
thickness,
elasticity_matrix,
alpha_t,
tfunc=None,
gauss_order=3):
from quadrature import legendre_quad
from shape_functions import iso_quad
from numpy import sum, array
freedom = 2
dimension = len(nodes) * freedom
force = zeros(dimension)
element_nodes = 4
(xi, eta, w) = legendre_quad(gauss_order)
alpha = array([alpha_t, alpha_t, 0.0])
for element in elements:
fe = zeros(element_nodes * freedom)
vertices = nodes[element[:], :]
for i in range(len(w)):
(jacobian, shape, shape_dx,
shape_dy) = iso_quad(vertices, xi[i], eta[i])
b = array([[
shape_dx[0], 0.0, shape_dx[1], 0.0, shape_dx[2], 0.0,
shape_dx[3], 0.0
],
[
0.0, shape_dy[0], 0.0, shape_dy[1], 0.0,
shape_dy[2], 0.0, shape_dy[3]
],
[
shape_dy[0], shape_dx[0], shape_dy[1], shape_dx[1],
shape_dy[2], shape_dx[2], shape_dy[3], shape_dx[3]
]])
if tfunc is None:
fe = fe + thickness * b.transpose().dot(elasticity_matrix).dot(
alpha) * w[i] * jacobian
else:
therm = tfunc(sum(vertices[:, 0] * shape),
sum(vertices[:, 1] * shape))
fe = fe + thickness * therm * b.transpose().dot(
elasticity_matrix).dot(alpha) * w[i] * jacobian
for i in range(element_nodes * freedom):
ii = element[i / freedom] * freedom + i % freedom
force[ii] += fe[i]
return force
def assembly_quads_stress_strain(nodes, elements, strain_stress_matrix, gauss_order=2):
"""
Assembly routine for plane stress-strain state analysis
:param nodes: Array of nodes coordinates
:param elements: Array of quads (mesh)
:param strain_stress_matrix: The stress-strain relations matrix
:param gauss_order: Order of gaussian quadratures
:return: Global stiffness matrix in the LIL sparse format (Row-based linked list sparse matrix)
Order: u_0, v0, u_1, v_1, ..., u_(n-1), v_(n-1), n - nodes count
"""
from numpy import zeros
from numpy import array
from quadrature import legendre_quad
from shape_functions import iso_quad
from scipy.sparse import lil_matrix
from print_progress import print_progress
print "Assembly is started"
freedom = 2
element_nodes = 4
nodes_count = len(nodes)
dimension = freedom * nodes_count
element_dimension = freedom * element_nodes
global_matrix = lil_matrix((dimension, dimension))
elements_count = len(elements)
(xi, eta, w) = legendre_quad(gauss_order)
for element_index in range(elements_count):
local = zeros((element_dimension, element_dimension))
for i in range(len(w)):
(jacobian, shape, shape_dx, shape_dy) = iso_quad(nodes, elements, element_index, xi[i], eta[i])
b = array([
[shape_dx[0], 0.0, shape_dx[1], 0.0, shape_dx[2], 0.0, shape_dx[3], 0.0],
[0.0, shape_dy[0], 0.0, shape_dy[1], 0.0, shape_dy[2], 0.0, shape_dy[3]],
[shape_dy[0], shape_dx[0], shape_dy[1], shape_dx[1], shape_dy[2], shape_dx[2], shape_dy[3], shape_dx[3]]
])
bt = b.conj().transpose()
local = local + bt.dot(strain_stress_matrix).dot(b) * jacobian * w[i]
for i in range(element_dimension):
ii = elements[element_index, i / freedom] * freedom + i % freedom
for j in range(i, element_dimension):
jj = elements[element_index, j / freedom] * freedom + j % freedom
global_matrix[ii, jj] += local[i, j]
if i != j:
global_matrix[jj, ii] = global_matrix[ii, jj]
print_progress(element_index, elements_count - 1)
print "\nAssembly is completed"
return global_matrix
[0.0, 0.000142857142857]
])
df = plane_stress_isotropic(e, nu)
dc = array([
[df[2, 2], 0.0],
[0.0, df[2, 2]]
])
(nodes, elements) = read('quad_triangle_mesh_21.txt')
stiffness = assembly_quads_mindlin_plate(nodes, elements, h, df, 5)
nodes_count = len(nodes)
dimension = freedom * nodes_count
element_dimension = freedom * element_nodes
geometric = lil_matrix((dimension, dimension))
(xi, eta, w) = legendre_quad(5)
for element in elements:
kg = zeros((element_dimension, element_dimension))
vertices = nodes[element[:], :]
for i in range(len(w)):
(jacobian, shape, shape_dx, shape_dy) = iso_quad(vertices, xi[i], eta[i])
bb = array([
[shape_dx[0], 0.0, 0.0, shape_dx[1], 0.0, 0.0, shape_dx[2], 0.0, 0.0, shape_dx[3], 0.0, 0.0],
[shape_dy[0], 0.0, 0.0, shape_dy[1], 0.0, 0.0, shape_dy[2], 0.0, 0.0, shape_dy[3], 0.0, 0.0]
])
bs1 = array([
[0.0, shape_dx[0], 0.0, 0.0, shape_dx[1], 0.0, 0.0, shape_dx[2], 0.0, 0.0, shape_dx[3], 0.0],
[0.0, shape_dy[0], 0.0, 0.0, shape_dy[1], 0.0, 0.0, shape_dy[2], 0.0, 0.0, shape_dy[3], 0.0]
])
def assembly_quads_mindlin_plate_geometric(nodes,
elements,
thickness,
sigma_x,
sigma_y,
tau_xy,
gauss_order=3):
from quadrature import legendre_quad
from shape_functions import iso_quad
from numpy import sum
print "The assembly routine is started"
freedom = 3
element_nodes = 4
nodes_count = len(nodes)
dimension = freedom * nodes_count
element_dimension = freedom * element_nodes
geometric = lil_matrix((dimension, dimension))
elements_count = len(elements)
(xi, eta, w) = legendre_quad(gauss_order)
for element_index in range(elements_count):
kg = zeros((element_dimension, element_dimension))
vertices = nodes[elements[element_index, :], :]
sx = sigma_x[elements[element_index, :]]
sy = sigma_y[elements[element_index, :]]
txy = tau_xy[elements[element_index, :]]
for i in range(len(w)):
(jacobian, shape, shape_dx,
shape_dy) = iso_quad(vertices, xi[i], eta[i])
s0 = array([[sum(shape * sx), sum(shape * txy)],
[sum(shape * txy), sum(shape * sy)]])
bb = array([[
shape_dx[0], 0.0, 0.0, shape_dx[1], 0.0, 0.0, shape_dx[2], 0.0,
0.0, shape_dx[3], 0.0, 0.0
],
[
shape_dy[0], 0.0, 0.0, shape_dy[1], 0.0, 0.0,
shape_dy[2], 0.0, 0.0, shape_dy[3], 0.0, 0.0
]])
bs1 = array([[
0.0, shape_dx[0], 0.0, 0.0, shape_dx[1], 0.0, 0.0, shape_dx[2],
0.0, 0.0, shape_dx[3], 0.0
],
[
0.0, shape_dy[0], 0.0, 0.0, shape_dy[1], 0.0, 0.0,
shape_dy[2], 0.0, 0.0, shape_dy[3], 0.0
]])
bs2 = array([[
0.0, 0.0, shape_dx[0], 0.0, 0.0, shape_dx[1], 0.0, 0.0,
shape_dx[2], 0.0, 0.0, shape_dx[3]
],
[
0.0, 0.0, shape_dy[0], 0.0, 0.0, shape_dy[1], 0.0,
0.0, shape_dy[2], 0.0, 0.0, shape_dy[3]
]])
kg = kg + thickness * bb.transpose().dot(s0).dot(
bb) * jacobian * w[i] + thickness**3.0 / 12.0 * (
bs1.transpose().dot(s0).dot(bs1) +
bs2.transpose().dot(s0).dot(bs2)) * jacobian * w[i]
for i in range(element_dimension):
ii = elements[element_index, i / freedom] * freedom + i % freedom
for j in range(i, element_dimension):
jj = elements[element_index,
j / freedom] * freedom + j % freedom
geometric[ii, jj] += kg[i, j]
if ii != jj:
geometric[jj, ii] = geometric[ii, jj]
print_progress(element_index, elements_count - 1)
print "\nThe assembly routine is completed"
return geometric.tocsr()
def assembly_quads_mindlin_plate_laminated(nodes,
elements,
thicknesses,
elasticity_matrices,
gauss_order=3,
kappa=5.0 / 6.0):
# type: (array, array, float, float, float, int, float) -> lil_matrix
"""
Assembly Routine for the Mindlin Plates Analysis
:param nodes: A two-dimensional array of plate's nodes coordinates
:param elements: A two-dimensional array of plate's triangles (mesh)
:param thicknesses: An array of thicknesses that stores thicknesses of each layer
:param elasticity_matrices: A list or a sequence of two-dimensional arrays. Each array represents stress-strain relations of corresponded layer
:param gauss_order: An order of gaussian quadratures
:param kappa: The shear correction factor
:return: Global stiffness matrix in the CSR sparse format
Order: u_0, v0, u_1, v_1, ..., u_(n-1), v_(n-1); n - nodes count
"""
from quadrature import legendre_quad
from shape_functions import iso_quad
from numpy import sum
print "The assembly routine is started"
freedom = 5
element_nodes = 4
nodes_count = len(nodes)
dimension = freedom * nodes_count
element_dimension = freedom * element_nodes
global_matrix = lil_matrix((dimension, dimension))
elements_count = len(elements)
(xi, eta, w) = legendre_quad(gauss_order)
h = sum(thicknesses)
for element_index in range(elements_count):
local = zeros((element_dimension, element_dimension))
element = nodes[elements[element_index, :], :]
for i in range(len(w)):
(jacobian, shape, shape_dx,
shape_dy) = iso_quad(element, xi[i], eta[i])
bm = array([[
shape_dx[0], 0.0, 0.0, 0.0, 0.0, shape_dx[1], 0.0, 0.0, 0.0,
0.0, shape_dx[2], 0.0, 0.0, 0.0, 0.0, shape_dx[3], 0.0, 0.0,
0.0, 0.0
],
[
0.0, shape_dy[0], 0.0, 0.0, 0.0, 0.0, shape_dy[1],
0.0, 0.0, 0.0, 0.0, shape_dy[2], 0.0, 0.0, 0.0,
0.0, shape_dy[3], 0.0, 0.0, 0.0
],
[
shape_dy[0], shape_dx[0], 0.0, 0.0, 0.0,
shape_dy[1], shape_dx[1], 0.0, 0.0, 0.0,
shape_dy[2], shape_dx[2], 0.0, 0.0, 0.0,
shape_dy[3], shape_dx[3], 0.0, 0.0, 0.0
]])
bf = array([[
0.0, 0.0, 0.0, shape_dx[0], 0.0, 0.0, 0.0, 0.0, shape_dx[1],
0.0, 0.0, 0.0, 0.0, shape_dx[2], 0.0, 0.0, 0.0, 0.0,
shape_dx[3], 0.0
],
[
0.0, 0.0, 0.0, 0.0, shape_dy[0], 0.0, 0.0, 0.0,
0.0, shape_dy[1], 0.0, 0.0, 0.0, 0.0, shape_dy[2],
0.0, 0.0, 0.0, 0.0, shape_dy[3]
],
[
0.0, 0.0, 0.0, shape_dy[0], shape_dx[0], 0.0, 0.0,
0.0, shape_dy[1], shape_dx[1], 0.0, 0.0, 0.0,
shape_dy[2], shape_dx[2], 0.0, 0.0, 0.0,
shape_dy[3], shape_dx[3]
]])
bc = array([[
0.0, 0.0, shape_dx[0], shape[0], 0.0, 0.0, 0.0, shape_dx[1],
shape[1], 0.0, 0.0, 0.0, shape_dx[2], shape[2], 0.0, 0.0, 0.0,
shape_dx[3], shape[3], 0.0
],
[
0.0, 0.0, shape_dy[0], 0.0, shape[0], 0.0, 0.0,
shape_dy[1], 0.0, shape[1], 0.0, 0.0, shape_dy[2],
0.0, shape[2], 0.0, 0.0, shape_dy[3], 0.0, shape[3]
]])
z0 = -h / 2.0
for j in range(len(thicknesses)):
z1 = z0 + thicknesses[j]
df = elasticity_matrices[j]
dc = array([[df[2, 2], 0.0], [0.0, df[2, 2]]])
local = local + (z1 - z0) * (
bm.transpose().dot(df).dot(bm)) * jacobian * w[i]
local = local + (z1**2.0 - z0**2.0) / 2.0 * (
bm.transpose().dot(df).dot(bf)) * jacobian * w[i]
local = local + (z1**2.0 - z0**2.0) / 2.0 * (
bf.transpose().dot(df).dot(bm)) * jacobian * w[i]
local = local + (z1**3.0 - z0**3.0) / 3.0 * (
bf.transpose().dot(df).dot(bf)) * jacobian * w[i]
local = local + (z1 - z0) * kappa * (
bc.transpose().dot(dc).dot(bc)) * jacobian * w[i]
z0 = z1
for i in range(element_dimension):
ii = elements[element_index, i / freedom] * freedom + i % freedom
for j in range(i, element_dimension):
jj = elements[element_index,
j / freedom] * freedom + j % freedom
global_matrix[ii, jj] += local[i, j]
if i != j:
global_matrix[jj, ii] = global_matrix[ii, jj]
print_progress(element_index, elements_count - 1)
print "\nThe assembly routine is completed"
return global_matrix.tocsr()