def on_calc_el_force(self, ex, ey, ed, element_type):
if element_type == 2:
es, et = cfc.plants(ex, ey, self.mesh.shape.ep, self.mesh.shape.D,
ed)
elMises = np.math.sqrt(
pow(es[0, 0], 2) - es[0, 0] * es[0, 1] + pow(es[0, 1], 2) +
3 * pow(es[0, 2], 2))
else:
es, et = cfc.planqs(ex, ey, self.mesh.shape.ep, self.mesh.shape.D,
ed)
elMises = np.math.sqrt(
pow(es[0], 2) - es[0] * es[1] + pow(es[1], 2) +
3 * pow(es[2], 2))
return elMises
print("Extracting ed...")
ed = cfc.extractEldisp(edof, a)
vonMises = []
# ---- Calculate elementr stresses and strains ------------------------------
print("Element forces... ")
for i in range(edof.shape[0]):
# Handle triangle elements
if elType == 2:
es, et = cfc.plants(ex[i,:], ey[i,:],
elprop[elementmarkers[i]][0],
elprop[elementmarkers[i]][1],
ed[i,:])
vonMises.append( np.math.sqrt( pow(es[0,0],2) - es[0,0]*es[0,1] + pow(es[0,1],2) + 3*pow(es[0,2],2) ) )
else:
# Handle quad elements
es, et = cfc.planqs(ex[i,:], ey[i,:],
elprop[elementmarkers[i]][0],
elprop[elementmarkers[i]][1],
ed[i,:])
vonMises.append( np.math.sqrt( pow(es[0],2) - es[0]*es[1] + pow(es[1],2) + 3*pow(es[2],2) ) )
def execute(self):
# ------ Transfer model variables to local variables
self.inputData.updateparams()
version = self.inputData.version
units = self.inputData.units
v = self.inputData.v
ep = self.inputData.ep
E = self.inputData.E
mp = self.inputData.mp
fp = self.inputData.fp
bp = self.inputData.bp
ep[1] = ep[1] * U2SI[units][0]
E = E * U2SI[units][2]
for i in range(len(fp[0])):
fp[1][i] = fp[1][i] * U2SI[units][1]
for i in range(len(bp[0])):
bp[1][i] = bp[1][i] * U2SI[units][0]
# Get most updated dxf dimensions and import model geometry to calfem format
self.inputData.dxf.readDXF(self.inputData.dxf_filename)
for dim in self.inputData.d:
("Adjusting Dimension {0} with val {1}".format(
dim[0], dim[1] * U2SI[units][0]))
self.inputData.dxf.adjustDimension(dim[0], dim[1] * U2SI[units][0])
self.inputData.dxf.adjustDimension(
self.inputData.c['aName'], self.inputData.c['a'] * U2SI[units][0])
self.inputData.dxf.adjustDimension(
self.inputData.c['bName'], self.inputData.c['b'] * U2SI[units][0])
dxf = self.inputData.dxf
if self.inputData.refineMesh:
geometry, curve_dict = dxf.convertToGeometry(max_el_size=mp[2])
else:
geometry, curve_dict = dxf.convertToGeometry()
# Generate the mesh
meshGen = cfm.GmshMeshGenerator(geometry)
meshGen.elSizeFactor = mp[2] # Max Area for elements
meshGen.elType = mp[0]
meshGen.dofsPerNode = mp[1]
meshGen.returnBoundaryElements = True
coords, edof, dofs, bdofs, elementmarkers, boundaryElements = meshGen.create(
)
# Add the force loads and boundary conditions
bc = np.array([], int)
bcVal = np.array([], int)
nDofs = np.size(dofs)
f = np.zeros([nDofs, 1])
for i in range(len(bp[0])):
bc, bcVal = cfu.applybc(bdofs, bc, bcVal, dxf.markers[bp[0][i]],
bp[1][i])
for i in range(len(fp[0])):
xforce = fp[1][i] * np.cos(np.radians(fp[2][i]))
yforce = fp[1][i] * np.sin(np.radians(fp[2][i]))
cfu.applyforce(bdofs,
f,
dxf.markers[fp[0][i]],
xforce,
dimension=1)
cfu.applyforce(bdofs,
f,
dxf.markers[fp[0][i]],
yforce,
dimension=2)
# ------ Calculate the solution
print("")
print("Solving the equation system...")
# Define the elements coordinates
ex, ey = cfc.coordxtr(edof, coords, dofs)
# Define the D and K matrices
D = (E / (1 - v**2)) * np.matrix([[1, v, 0], [v, 1, 0],
[0, 0, (1 - v) / 2]])
K = np.zeros([nDofs, nDofs])
# Extract element coordinates and topology for each element
for eltopo, elx, ely in zip(edof, ex, ey):
Ke = cfc.plante(elx, ely, ep, D)
cfc.assem(eltopo, K, Ke)
# Solve the system
a, r = cfc.solveq(K, f, bc, bcVal)
# ------ Determine stresses and displacements
print("Computing the element forces")
# Extract element displacements
ed = cfc.extractEldisp(edof, a)
# Determine max displacement
max_disp = [[0, 0], 0] # [node idx, value]
for idx, node in zip(range(len(ed)), ed):
for i in range(3):
disp = math.sqrt(node[2 * i]**2 + node[2 * i + 1]**2)
if disp > max_disp[1]:
max_disp = [[idx, 2 * i], disp]
# Determine Von Mises stresses
vonMises = []
max_vm = [0, 0] # [node idx, value]
for i in range(edof.shape[0]):
es, et = cfc.plants(ex[i, :], ey[i, :], ep, D, ed[i, :])
try:
vonMises.append(
math.sqrt(
pow(es[0, 0], 2) - es[0, 0] * es[0, 1] +
pow(es[0, 1], 2) + 3 * es[0, 2]))
if vonMises[-1] > max_vm[1]:
max_vm = [i, vonMises[-1]]
except ValueError:
vonMises.append(0)
print("CAUGHT MATH EXCEPTION with es = {0}".format(es))
# Note: es = [sigx sigy tauxy]
# ------ Store the solution in the output model variables
self.outputData.disp = ed
self.outputData.stress = vonMises
self.outputData.geometry = geometry
self.outputData.a = a
self.outputData.coords = coords
self.outputData.edof = edof
self.outputData.mp = mp
self.outputData.meshGen = meshGen
self.outputData.statistics = [
max_vm, max_disp, curve_dict, self.inputData.dxf.anchor,
self.inputData.dxf.wh
]
if self.inputData.paramFilename is None:
print("Solution completed.")
cfu.info("Extracting ed...")
ed = cfc.extractEldisp(edof, a)
von_mises = []
# ---- Calculate elementr stresses and strains ------------------------------
cfu.info("Element forces... ")
for i in range(edof.shape[0]):
# Handle triangle elements
if el_type == 2:
es, et = cfc.plants(ex[i,:], ey[i,:],
elprop[elementmarkers[i]][0],
elprop[elementmarkers[i]][1],
ed[i,:])
von_mises.append( np.math.sqrt( pow(es[0,0],2) - es[0,0]*es[0,1] + pow(es[0,1],2) + 3*pow(es[0,2],2) ) )
else:
# Handle quad elements
es, et = cfc.planqs(ex[i,:], ey[i,:],
elprop[elementmarkers[i]][0],
elprop[elementmarkers[i]][1],
ed[i,:])
von_mises.append( np.math.sqrt( pow(es[0],2) - es[0]*es[1] + pow(es[1],2) + 3*pow(es[2],2) ) )