def getMembranePlateMaterials(preprocessor):
''' return a dictionary with the XC materials for shell elements.'''
retval = dict()
for key in steel_dict:
steelType = steel_dict[key]
#retval[key]= typical_materials.defElasticMembranePlateSection(preprocessor, 'xc_'+key,steelType.E,steelType.nu,7850.0,h= 0.0)
steel3DName = '3Dmat_' + key
steel3d = typical_materials.defElasticIsotropic3d(preprocessor,
steel3DName,
steelType.E,
steelType.nu,
rho=steelType.rho)
retval[steel3DName] = steel3d
plateFiberName = 'plateFiber_' + key
# Thickness is assigned later for each element.
plateFiber = typical_materials.defMembranePlateFiberSection(
preprocessor, name=plateFiberName, h=0.0, nDMaterial=steel3d)
retval[key] = plateFiber
return retval
__license__ = "GPL"
__version__ = "3.0"
__email__ = "*****@*****.**"
import xc_base
import geom
import xc
from solution import predefined_solutions
from model import predefined_spaces
from materials import typical_materials
# Problem type
feProblem = xc.FEProblem()
preprocessor = feProblem.getPreprocessor
# Materials definition
elast = typical_materials.defElasticIsotropic3d(preprocessor, "elast3d", 1e6,
0.25, 0.0)
nodes = preprocessor.getNodeLoader
modelSpace = predefined_spaces.SolidMechanics3D(nodes)
nod1 = nodes.newNodeXYZ(0.249, 0.342, 0.192)
nod2 = nodes.newNodeXYZ(0.826, 0.288, 0.288)
nod3 = nodes.newNodeXYZ(0.850, 0.649, 0.263)
nod4 = nodes.newNodeXYZ(0.273, 0.750, 0.230)
nod5 = nodes.newNodeXYZ(0.320, 0.186, 0.643)
nod6 = nodes.newNodeXYZ(0.677, 0.305, 0.683)
nod7 = nodes.newNodeXYZ(0.788, 0.693, 0.644)
nod8 = nodes.newNodeXYZ(0.165, 0.745, 0.702)
nod9 = nodes.newNodeXYZ(0, 0, 0)
nod10 = nodes.newNodeXYZ(1, 0, 0)
nod11 = nodes.newNodeXYZ(1, 1, 0)
nod12 = nodes.newNodeXYZ(0, 1, 0)
__license__ = "GPL"
__version__ = "3.0"
__email__ = "*****@*****.**"
import xc_base
import geom
import xc
from solution import predefined_solutions
from model import predefined_spaces
from materials import typical_materials
# Problem type
feProblem = xc.FEProblem()
preprocessor = feProblem.getPreprocessor
# Materials definition
elast = typical_materials.defElasticIsotropic3d(preprocessor, "elast3d",
200000, 0.3, 0.0)
nodes = preprocessor.getNodeHandler
modelSpace = predefined_spaces.SolidMechanics3D(nodes)
nodes.defaultTag = 1 #Next node number.
nod1 = nodes.newNodeXYZ(100, 0, 100)
nod2 = nodes.newNodeXYZ(0, 0, 100)
nod3 = nodes.newNodeXYZ(0, 0, 200)
nod4 = nodes.newNodeXYZ(100, 0, 200)
nod5 = nodes.newNodeXYZ(100, 100, 100)
nod6 = nodes.newNodeXYZ(0, 100, 100)
nod7 = nodes.newNodeXYZ(0, 100, 200)
nod8 = nodes.newNodeXYZ(100, 100, 200)
nod9 = nodes.newNodeXYZ(100, 200, 100)
nod10 = nodes.newNodeXYZ(0, 200, 100)
elements = prep.getElementHandler
elements.dimElem = 3
modelSpace = predefined_spaces.StructuralMechanics3D(nodes)
gridGeom = gm.GridModel(prep, rList, angList, zList, xCentCoo=0, yCentCoo=0)
gridGeom.generateCylZPoints()
ring = gridGeom.genSurfOneXYZRegion([(r1, 0, 0), (r2, angList[-1], 0)],
setName='ring',
closeCyl='Y')
#out=outHndl.OutputHandler(modelSpace)
#out.displayBlocks()
steel = tm.defElasticIsotropic3d(preprocessor=preprocessor,
name='steel',
E=172e9,
nu=0.3,
rho=matRho)
ring_mat = tm.defMembranePlateFiberSection(preprocessor,
name='ring_mat',
h=t,
nDMaterial=steel)
ring_mesh = fem.SurfSetToMesh(surfSet=ring,
matSect=ring_mat,
elemSize=0.5,
elemType='ShellMITC4')
fem.multi_mesh(prep, [ring_mesh])
# Constraints
xcTotalSet = modelSpace.getTotalSet()
constrainedNodes = list()
n30 = nodes.newNodeXYZ(9.0, 0., 0.)
n31 = nodes.newNodeXYZ(10., 1., 0.)
n32 = nodes.newNodeXYZ(10., 0.5, 0.)
n33 = nodes.newNodeXYZ(10., 0., 0.)
# Constraints.
constrainedNodes = [n1, n2, n3]
for n in constrainedNodes:
modelSpace.fixNode000_000(n.tag)
# Materials
E = 1.2e6
nu = 0.3
elast3d = typical_materials.defElasticIsotropic3d(preprocessor,
"elast3d",
E,
nu,
rho=0.0)
thickness = 0.1
plateFiber = typical_materials.defMembranePlateFiberSection(preprocessor,
name="plateFiber",
h=thickness,
nDMaterial=elast3d)
## Full circle moment
I = 1 / 12.0 * 1.0 * thickness**3
L = 10.0 # lenght of the beam
Mcircle = 2.0 * math.pi * E * I / L
# Elements
elements = preprocessor.getElementHandler
elements.defaultMaterial = plateFiber.name
A = h * h # bar area expressed in square meters
I = (h)**4 / 12 # Cross section moment of inertia (m4)
AT = 10.0 # Temperature increment (Celsius degrees)
feProblem = xc.FEProblem()
preprocessor = feProblem.getPreprocessor
nodes = preprocessor.getNodeHandler
modelSpace = predefined_spaces.StructuralMechanics3D(nodes)
nodes.defaultTag = 1 # First node number.
nod1 = nodes.newNodeXYZ(0.0, 0.0, 0.0)
nod2 = nodes.newNodeXYZ(L, 0.0, 0.0)
nod3 = nodes.newNodeXYZ(L, h, 0.0)
nod4 = nodes.newNodeXYZ(0, h, 0.0)
# Materials definition
ndMat = typical_materials.defElasticIsotropic3d(preprocessor, "elastIso3d", E,
0.3, 0.0)
memb1 = typical_materials.defMembranePlateFiberSection(preprocessor,
name='memb1',
h=h,
nDMaterial=ndMat)
# Elements definition
elements = preprocessor.getElementHandler
elements.defaultMaterial = memb1.name
elem1 = elements.newElement("ShellMITC4",
xc.ID([nod1.tag, nod2.tag, nod3.tag, nod4.tag]))
# Constraints
constraints = preprocessor.getBoundaryCondHandler
spc = constraints.newSPConstraint(nod1.tag, 0, 0.0)
# Home made test __author__= "Luis C. Pérez Tato (LCPT) and Ana Ortega (AOO)" __copyright__= "Copyright 2015, LCPT and AOO" __license__= "GPL" __version__= "3.0" __email__= "*****@*****.**" E= 30e6 # Young modulus (psi) nu= 0.33 # Poisson's ratio rho= 1.5 # Density import xc_base import geom import xc from model import predefined_spaces from materials import typical_materials # Define materials feProblem= xc.FEProblem() preprocessor= feProblem.getPreprocessor mat= typical_materials.defElasticIsotropic3d(preprocessor, "elastIso3d",E,nu,rho) import os from miscUtils import LogMessages as lmsg fname= os.path.basename(__file__) if (abs(mat.E-E)<1e-15) & (abs(mat.nu-nu)<1e-15) & (abs(mat.rho-rho)<1e-15): print "test ",fname,": ok." else: lmsg.error(fname+' ERROR.')
__license__ = "GPL"
__version__ = "3.0"
__email__ = "*****@*****.**"
import xc_base
import geom
import xc
from model import predefined_spaces
from materials import typical_materials
from postprocess import output_handler
# Problem type
feProblem = xc.FEProblem()
preprocessor = feProblem.getPreprocessor
# Materials definition
concrete = typical_materials.defElasticIsotropic3d(preprocessor, "concrete3d",
28.3e9, 0.2, 0.0)
# Geometry
width = 6 * 0.0254
length = 4 * 0.3048
height = 12 * 0.0254
## Block topology
points = preprocessor.getMultiBlockTopology.getPoints
pt1 = points.newPntFromPos3d(geom.Pos3d(0.0, 0.0, 0.0))
pt2 = points.newPntFromPos3d(geom.Pos3d(width, 0.0, 0.0))
pt3 = points.newPntFromPos3d(geom.Pos3d(width, length, 0.0))
pt4 = points.newPntFromPos3d(geom.Pos3d(0.0, length, 0.0))
pt5 = points.newPntFromPos3d(geom.Pos3d(0.0, 0.0, height))
__license__= "GPL" __version__= "3.0" __email__= "*****@*****.**" import xc_base import geom import xc from solution import predefined_solutions from model import predefined_spaces from materials import typical_materials # Problem type feProblem= xc.FEProblem() preprocessor= feProblem.getPreprocessor # Materials definition elast= typical_materials.defElasticIsotropic3d(preprocessor, "elast3d",1e6,0.25,0.0) nodes= preprocessor.getNodeHandler modelSpace= predefined_spaces.SolidMechanics3D(nodes) nod9= nodes.newNodeIDXYZ(9,0,0,0) nod10= nodes.newNodeIDXYZ(10,1,0,0) nod11= nodes.newNodeIDXYZ(11,1,1,0) nod12= nodes.newNodeIDXYZ(12,0,1,0) nod13= nodes.newNodeIDXYZ(13,0,0,1) nod14= nodes.newNodeIDXYZ(14,1,0,1) nod15= nodes.newNodeIDXYZ(15,1,1,1) nod16= nodes.newNodeIDXYZ(16,0,1,1) elements= preprocessor.getElementHandler elements.defaultMaterial= "elast3d"
# Problem type
feProblem = xc.FEProblem()
preprocessor = feProblem.getPreprocessor
nodes = preprocessor.getNodeHandler
modelSpace = predefined_spaces.StructuralMechanics3D(nodes)
# Material definition
## Steel material
steel = ASTM_materials.A992
steel.gammaM = 1.00
sg_yield = steel.fy # Allowable stress: yield stress of steel (Pa)
## XC material model
steel3d = typical_materials.defElasticIsotropic3d(preprocessor,
"steel3d",
steel.E,
steel.nu,
rho=steel.rho)
plateFiber = typical_materials.defMembranePlateFiberSection(preprocessor,
name="plateFiber",
h=t,
nDMaterial=steel3d)
# Problem geometry
# The “bottom-up method” generates the geometry of the system
# going from key points (0D) to lines (1D) and areas (2D)
# up to volumes (3D).
p1 = modelSpace.newKPoint(0.0, h / 2.0)
p2 = modelSpace.newKPoint(L / 2.0, h / 2.0)
__license__= "GPL" __version__= "3.0" __email__= "*****@*****.**" import xc_base import geom import xc from solution import predefined_solutions from model import predefined_spaces from materials import typical_materials # Problem type feProblem= xc.FEProblem() preprocessor= feProblem.getPreprocessor # Materials definition elast= typical_materials.defElasticIsotropic3d(preprocessor, "elast3d",200000,0.3,0.0) nodes= preprocessor.getNodeHandler modelSpace= predefined_spaces.SolidMechanics3D(nodes) nodes.defaultTag= 1 #Next node number. nod1= nodes.newNodeXYZ(100,0,100) nod2= nodes.newNodeXYZ(0,0,100) nod3= nodes.newNodeXYZ(0,0,200) nod4= nodes.newNodeXYZ(100,0,200) nod5= nodes.newNodeXYZ(100,100,100) nod6= nodes.newNodeXYZ(0,100,100) nod7= nodes.newNodeXYZ(0,100,200) nod8= nodes.newNodeXYZ(100,100,200) nod9= nodes.newNodeXYZ(100,200,100) nod10= nodes.newNodeXYZ(0,200,100)