def def_secc_aggregation2d(preprocessor,defSecc,defMat):
''' Definition of a elastic material-section for 2D elements
:param preprocessor: preprocessor name
:param defSecc: object with the mechanical properties of the section (A, Iy, Iz, ...)
:param defMat: object with the properties of the material (E, G)
'''
nmbRigF= defSecc.sectionName+ "_rigF" # Bending stiffness.
typical_materials.defElasticSection2d(preprocessor,nmbRigF,defSecc.A(),defMat.E,defSecc.Iz())
nmbRigVy= defSecc.sectionName+"_rigVy" # Y shear stiffness.
typical_materials.defElasticMaterial(preprocessor,nmbRigVy,defSecc.alphaY()*defMat.G()*defSecc.A())
materialHandler= preprocessor.getMaterialHandler
agg= materialHandler.newMaterial("section_aggregator",defSecc.sectionName)
agg.setSection(nmbRigF)
agg.setAdditions(["Vy"],[nmbRigVy])
def defElasticSection2d(self, preprocessor, material):
''' Return an elastic section appropiate for 2D beam analysis,
including shear deformations
:param preprocessor: preprocessor object.
:param material: material constitutive model (for which
E is the Young's modulus)
'''
if (not self.xc_material):
materialHandler = preprocessor.getMaterialHandler
if (materialHandler.materialExists(self.sectionName)):
lmsg.warning("Section: " + self.sectionName +
" already defined.")
self.xc_material = materialHandler.getMaterial(
self.sectionName)
else:
self.xc_material = typical_materials.defElasticSection2d(
preprocessor,
self.sectionName,
self.A(),
material.E,
self.Iz(),
rho=material.rho)
else:
lmsg.warning('Material: ' + self.sectionName +
' already defined as:' + str(self.xc_material))
return self.xc_material
def defElasticSection2d(self, preprocessor, material, majorAxis=True):
''' Return an elastic section appropiate for 2D beam analysis
:param preprocessor: preprocessor object.
:param material: material constitutive model
(for which E is the Young's modulus)
:param majorAxis: true if bending occurs in the section major axis.
'''
if (not self.xc_material):
materialHandler = preprocessor.getMaterialHandler
if (materialHandler.materialExists(self.sectionName)):
lmsg.warning("Section: " + self.sectionName +
" already defined.")
self.xc_material = materialHandler.getMaterial(
self.sectionName)
else:
I = self.Iz()
if (not majorAxis):
I = self.Iy()
self.xc_material = typical_materials.defElasticSection2d(
preprocessor,
self.sectionName,
self.A(),
material.E,
I,
linearRho=material.rho * self.A())
else:
lmsg.warning('Material: ' + self.sectionName +
' already defined as:' + str(self.xc_material))
return self.xc_material
def defSeccAggregation2d(preprocessor, defSecc, defMat):
''' Definition of a elastic material-section for 2D elements
:param preprocessor: preprocessor name
:param defSecc: object with the mechanical properties of the section (A, Iy, Iz, ...)
:param defMat: object with the properties of the material (E, G)
'''
nmbRigF = defSecc.nmb + "_rigF" # Rigidez a flexión.
typical_materials.defElasticSection2d(preprocessor, nmbRigF, defSecc.A(),
defMat.E, defSecc.Iz())
nmbRigVy = defSecc.nmb + "_rigVy" # Rigidez a cortante y.
typical_materials.defElasticMaterial(
preprocessor, nmbRigVy,
defSecc.alphaY() * defMat.G() * defSecc.A())
materiales = preprocessor.getMaterialLoader
agg = materiales.newMaterial("section_aggregator", defSecc.nmb)
agg.setSection(nmbRigF)
agg.setAdditions(["Vy"], [nmbRigVy])
def defElasticSection2d(self,preprocessor,material):
'''elastic section appropiate for 2D beam analysis, including shear deformations
:param preprocessor: preprocessor object.
:param material: material constitutive model (for which
E is the Young's modulus)
'''
materiales= preprocessor.getMaterialLoader
if(materiales.materialExists(self.sectionName)):
sys.stderr.write("Section: "+self.sectionName+" is already defined.")
else:
retval= typical_materials.defElasticSection2d(preprocessor,self.sectionName,self.A(),material.E,self.Iz())
return retval
def defElasticSection2d(self,preprocessor,material):
'''elastic section appropiate for 2D beam analysis, including shear deformations
:param preprocessor: preprocessor object.
:param material: material constitutive model (for which
E is the Young's modulus)
'''
materiales= preprocessor.getMaterialHandler
if(materiales.materialExists(self.sectionName)):
sys.stderr.write("Section: "+self.sectionName+" is already defined.")
else:
retval= typical_materials.defElasticSection2d(preprocessor,self.sectionName,self.A(),material.E,self.Iz())
return retval
nod4.mass = nodeMassMatrix
nod4.setProp("gdlsCoartados", xc.ID([1, 2]))
nod5 = nodes.newNodeXY(0, 4 + 3 + 3 + 3 + 3)
nod5.mass = nodeMassMatrix
nod5.setProp("gdlsCoartados", xc.ID([1, 2]))
setTotal = preprocessor.getSets.getSet("total")
nodes = setTotal.getNodes
for n in nodes:
n.fix(n.getProp("gdlsCoartados"), xc.Vector([0, 0, 0]))
# Materials definition
materialHandler = preprocessor.getMaterialHandler
#scc= typical_materials.defElasticSection2d(preprocessor, "scc",A,E,I)
sccPlBaja = typical_materials.defElasticSection2d(preprocessor, "sccPlBaja",
20 * Bbaja * Bbaja, Ehorm,
20 * Ibaja)
sccPl1a = typical_materials.defElasticSection2d(preprocessor, "sccPl1a",
20 * B1a * B1a, Ehorm,
20 * I1a)
sccPl2a = typical_materials.defElasticSection2d(preprocessor, "sccPl2a",
20 * B1a * B1a, Ehorm,
20 * I1a)
sccPl3a = typical_materials.defElasticSection2d(preprocessor, "sccPl3a",
20 * B3a * B3a, Ehorm,
20 * I3a)
sccPl4a = typical_materials.defElasticSection2d(preprocessor, "sccPl4a",
20 * B3a * B3a, Ehorm,
20 * I3a)
# Geometric transformation(s)
# Problem type
modelSpace = predefined_spaces.StructuralMechanics2D(nodes)
# Definimos el material
def_secc_aggregation.def_secc_aggregation2d(preprocessor, sectionTest,
sectionTestMaterial)
nodes.defaultTag = 1 # First node number.
nod = nodes.newNodeXY(0, 0)
nod = nodes.newNodeXY(L, 0.0)
# Geometric transformations
lin = modelSpace.newLinearCrdTransf("lin")
# Materials definition
scc = typical_materials.defElasticSection2d(preprocessor, "scc",
sectionTest.A(),
sectionTestMaterial.E,
sectionTest.Iz())
# Elements definition
elements = preprocessor.getElementHandler
elements.defaultTransformation = lin.name
elements.defaultMaterial = scc.name
elements.defaultMaterial = sectionTest.sectionName
elements.numSections = 3 # Number of sections along the element.
elements.defaultTag = 1
beam2d = elements.newElement("ForceBeamColumn2d", xc.ID([1, 2]))
# Constraints
constraints = preprocessor.getBoundaryCondHandler
modelSpace.fixNode000(1)
h= 0.2 # Cross section depth in meters
A= b*h # Cross section area en m2
I= 1/12.0*b*h**3 # Moment of inertia in m4
E=1e4/I # Elastic modulus en N/m2
P= -100 # Carga vertical sobre la columna.
NumDiv= 4
# Problem type
feProblem= xc.FEProblem()
preprocessor= feProblem.getPreprocessor
nodes= preprocessor.getNodeHandler
modelSpace= predefined_spaces.StructuralMechanics2D(nodes)
# Materials definition
scc= typical_materials.defElasticSection2d(preprocessor, "scc",A,E,I)
nodes.newSeedNode()
# Geometric transformation(s)
lin= modelSpace.newPDeltaCrdTransf("lin")
# Seed element definition
seedElemHandler= preprocessor.getElementHandler.seedElemHandler
seedElemHandler.defaultMaterial= "scc"
seedElemHandler.defaultTransformation= "lin"
seedElemHandler.defaultTag= 1 #Tag for next element.
beam2d= seedElemHandler.newElement("ElasticBeam2d",xc.ID([0,0]))
beam2d.h= h
beam2d.rho= 0.0
import geom
import xc
from solution import predefined_solutions
from model import predefined_spaces
from materials import typical_materials
feProblem= xc.FEProblem()
preprocessor= feProblem.getPreprocessor
nodes= preprocessor.getNodeHandler
modelSpace= predefined_spaces.StructuralMechanics2D(nodes)
pd= modelSpace.newPDeltaCrdTransf("pd")
# Materials definition
scc= typical_materials.defElasticSection2d(preprocessor, "scc",area,Es,Iz)
seedElemHandler= preprocessor.getElementHandler.seedElemHandler
seedElemHandler.defaultMaterial= scc.name
seedElemHandler.defaultTransformation= pd.name
seedElemHandler.defaultTag= 1 #Tag for next element.
beam2d= seedElemHandler.newElement("ElasticBeam2d",xc.ID([1,2]))
points= preprocessor.getMultiBlockTopology.getPoints
pt1= points.newPntIDPos3d(1, geom.Pos3d(0.0,0.0,0))
pt2= points.newPntIDPos3d(2, geom.Pos3d(0.0,H,0))
pt3= points.newPntIDPos3d(3, geom.Pos3d(B,0.0,0))
pt4= points.newPntIDPos3d(4, geom.Pos3d(B,H,0))
pt5= points.newPntIDPos3d(5, geom.Pos3d(offset,0.0,0))
pt6= points.newPntIDPos3d(6, geom.Pos3d(offset,H,0))
pt7= points.newPntIDPos3d(7, geom.Pos3d(offset+B,0.0,0))
nod4= nodes.newNodeXY(0,4+3+3)
nod4.mass= nodeMassMatrix
nod4.setProp("gdlsCoartados",xc.ID([1,2]))
nod5= nodes.newNodeXY(0,4+3+3+3)
nod5.mass= nodeMassMatrix
nod5.setProp("gdlsCoartados",xc.ID([1,2]))
nod6= nodes.newNodeXY(0,4+3+3+3+3)
nod6.mass= nodeMassMatrix
nod6.setProp("gdlsCoartados",xc.ID([1,2]))
setTotal= preprocessor.getSets["total"]
nodes= setTotal.getNodes
for n in nodes:
n.fix(n.getProp("gdlsCoartados"),xc.Vector([0,0,0]))
# Materials definition
sccPlBaja= typical_materials.defElasticSection2d(preprocessor, "sccPlBaja",20*Bbaja*Bbaja,Ehorm,20*Ibaja)
sccPl1a= typical_materials.defElasticSection2d(preprocessor, "sccPl1a",20*B1a*B1a,Ehorm,20*I1a)
sccPl2a= typical_materials.defElasticSection2d(preprocessor, "sccPl2a",20*B1a*B1a,Ehorm,20*I1a)
sccPl3a= typical_materials.defElasticSection2d(preprocessor, "sccPl3a",20*B3a*B3a,Ehorm,20*I3a)
sccPl4a= typical_materials.defElasticSection2d(preprocessor, "sccPl4a",20*B3a*B3a,Ehorm,20*I3a)
# Geometric transformation(s)
lin= modelSpace.newLinearCrdTransf("lin")
# Elements definition
elements= preprocessor.getElementHandler
elements.defaultTransformation= "lin"
elements.defaultMaterial= "sccPlBaja"
elements.defaultTag= 1 #Tag for next element.
beam2d= elements.newElement("ElasticBeam2d",xc.ID([0,1]))
L = 20 # Bar length.
# Problem type
feProblem = xc.FEProblem()
preprocessor = feProblem.getPreprocessor
nodes = preprocessor.getNodeHandler
modelSpace = predefined_spaces.StructuralMechanics2D(nodes)
nodes.defaultTag = 1 #First node number.
nod = nodes.newNodeXY(0, 0)
nod = nodes.newNodeXY(L * math.sqrt(2) / 2, L * math.sqrt(2) / 2)
# Geometric transformations
lin = modelSpace.newLinearCrdTransf("lin")
# Materials
section = typical_materials.defElasticSection2d(preprocessor, "section", 1, 1,
1)
# Elements definition
elements = preprocessor.getElementHandler
elements.defaultTransformation = lin.name
elements.defaultMaterial = section.name
# sintaxis: beam2d_02[<tag>]
elements.defaultTag = 1 #Tag for next element.
beam2d = elements.newElement("ElasticBeam2d", xc.ID([1, 2]))
coordTransf = beam2d.getCoordTransf
centroideG = coordTransf.getPointGlobalCoordFromBasic(0.5)
posCentroideG = geom.Pos2d(centroideG[0], centroideG[1])
centroideL = coordTransf.getPointLocalCoordFromGlobal(centroideG)
posCentroideL = geom.Pos2d(centroideL[0], centroideL[1])
centroideB = coordTransf.getPointBasicCoordFromGlobal(centroideG)
nodes = preprocessor.getNodeHandler
# Problem type
modelSpace = predefined_spaces.StructuralMechanics2D(nodes)
nodes.defaultTag = 0 #First node number.
nod = nodes.newNodeXY(0, 0)
nod = nodes.newNodeXY(1.0, 0.0)
nod = nodes.newNodeXY(2.0, 0.0)
# Geometric transformations
trfs = preprocessor.getTransfCooHandler
lin = trfs.newLinearCrdTransf2d("lin")
# Materials definition
scc = typical_materials.defElasticSection2d(
preprocessor, "scc", beamRCsect.lstRCSects[0].getAc(),
beamRCsect.lstRCSects[0].fiberSectionParameters.concrType.Ecm(),
beamRCsect.lstRCSects[0].getI())
#print scc.sectionProperties.I
# Elements definition
elementos = preprocessor.getElementHandler
elementos.defaultTransformation = "lin"
elementos.defaultMaterial = "scc"
# sintaxis: beam2d_02[<tag>]
elementos.defaultTag = 1 #Tag for next element.
beam2dA = elementos.newElement("ElasticBeam2d", xc.ID([0, 1]))
beam2dA.h = hbeam
beam2dB = elementos.newElement("ElasticBeam2d", xc.ID([1, 2]))
beam2dB.h = hbeam
# Problem type
modelSpace = predefined_spaces.StructuralMechanics2D(nodes)
# Definimos el material
defSeccAggregation.defSeccAggregation2d(preprocessor, seccPrueba,
matSeccPrueba)
nodes.defaultTag = 1 #First node number.
nod = nodes.newNodeXY(0, 0)
nod = nodes.newNodeXY(L, 0.0)
# Geometric transformations
trfs = preprocessor.getTransfCooLoader
lin = trfs.newLinearCrdTransf2d("lin")
# Materials definition
scc = typical_materials.defElasticSection2d(preprocessor, "scc",
seccPrueba.A(), matSeccPrueba.E,
seccPrueba.Iz())
# Elements definition
elementos = preprocessor.getElementLoader
elementos.defaultTransformation = "lin"
elementos.defaultMaterial = "scc"
elementos.defaultMaterial = seccPrueba.nmb
elementos.numSections = 3 # Número de secciones a lo largo del elemento.
elementos.defaultTag = 1
beam2d = elementos.newElement("force_beam_column_2d", xc.ID([1, 2]))
# Constraints
coacciones = preprocessor.getConstraintLoader
fix_node_3dof.fixNode000(coacciones, 1)
#three DOF for each node (Ux,Uy,Theta)
## *** MESH ***
### *** GEOMETRY ***
n1 = nodes.newNodeXY(0.0, 0.0)
n2 = nodes.newNodeXY(0.0, 432.0)
### Single point constraints -- Boundary Conditions
constraints = prep.getBoundaryCondHandler
modelSpace.fixNode000(n1.tag)
### nodal masses:
n2.mass = xc.Matrix([[5.18, 0, 0], [0, 0, 0], [0, 0, 0]]) # node mass matrix.
### Define materials.
beamSection = typical_materials.defElasticSection2d(prep, "beamSection", 3600,
1080000, 3225)
### Define ELEMENTS
# define geometric transformation: performs a linear geometric transformation
# of beam stiffness and resisting force from the basic system to the
# global-coordinate system
lin = modelSpace.newLinearCrdTransf("lin")
elements = prep.getElementHandler
elements.defaultTransformation = lin.name
elements.defaultMaterial = beamSection.name
beam2d = elements.newElement("ElasticBeam2d", xc.ID([n1.tag, n2.tag]))
## *** Loads ***
### define GRAVITY -------------------------------------------------------------
loadPatterns = prep.getLoadHandler.getLoadPatterns
gravityTS = loadPatterns.newTimeSeries("constant_ts", "ts")
import xc_base
import geom
import xc
from solution import predefined_solutions
from model import predefined_spaces
from materials import typical_materials
feProblem= xc.FEProblem()
preprocessor= feProblem.getPreprocessor
nodes= preprocessor.getNodeHandler
modelSpace= predefined_spaces.StructuralMechanics2D(nodes)
nodes.newSeedNode()
# Materials definition
scc= typical_materials.defElasticSection2d(preprocessor, "scc",area,Es,Iz)
pd= modelSpace.newPDeltaCrdTransf("pd")
seedElemHandler= preprocessor.getElementHandler.seedElemHandler
seedElemHandler.defaultTransformation= "pd"
seedElemHandler.defaultMaterial= "scc"
seedElemHandler.defaultTag= 1 #Tag for next element.
beam2d= seedElemHandler.newElement("ElasticBeam2d",xc.ID([0,0]))
points= preprocessor.getMultiBlockTopology.getPoints
pt1= points.newPntIDPos3d(1, geom.Pos3d(0.0,0.0,0) )
pt2= points.newPntIDPos3d(2, geom.Pos3d(0.0,H,0) )
pt3= points.newPntIDPos3d(3, geom.Pos3d(B,0.0,0) )
pt4= points.newPntIDPos3d(4, geom.Pos3d(B,H,0) )
pt5= points.newPntIDPos3d(5, geom.Pos3d(offset,0.0,0) )
nod = nodes.newNodeXY(0, 0)
nod = nodes.newNodeXY(1.0, 0.0)
nod = nodes.newNodeXY(2.0, 0.0)
# Geometric transformations
trfs = preprocessor.getTransfCooHandler
lin = trfs.newLinearCrdTransf2d("lin")
# Materials definition
# A: cross-sectional area of the section
# E: Young’s modulus of material
# I: second moment of area about the local z-axis
scc = typical_materials.defElasticSection2d(
preprocessor=preprocessor,
name="scc",
A=beamRCsect.lstRCSects[0].getAc(),
E=beamRCsect.lstRCSects[0].concrType.Ecm(),
I=beamRCsect.lstRCSects[0].getI())
# Elements definition
elementos = preprocessor.getElementHandler
elementos.defaultTransformation = "lin"
elementos.defaultMaterial = "scc"
# sintaxis: beam2d_02[<tag>]
elementos.defaultTag = 1 #Tag for next element.
beam2dA = elementos.newElement("ElasticBeam2d", xc.ID([0, 1]))
beam2dA.h = hbeam
beam2dB = elementos.newElement("ElasticBeam2d", xc.ID([1, 2]))
beam2dB.h = hbeam
# Constraints
__version__= "3.0"
__email__= "*****@*****.**"
# Problem type
feProblem= xc.FEProblem()
preprocessor= feProblem.getPreprocessor
nodes= preprocessor.getNodeHandler
modelSpace= predefined_spaces.StructuralMechanics2D(nodes)
nodes.defaultTag= 1 #First node number.
nod= nodes.newNodeXY(0,0)
nod= nodes.newNodeXY(5,5)
# Geometric transformations
lin= modelSpace.newLinearCrdTransf("lin")
# Materials
section= typical_materials.defElasticSection2d(preprocessor, "section",1,1,1)
# Elements definition
elements= preprocessor.getElementHandler
elements.defaultTransformation= "lin" # Coordinate transformation for the new elements
elements.defaultMaterial= "section"
elements.defaultTag= 1 #Tag for next element.
beam2d= elements.newElement("ElasticBeam2d",xc.ID([1,2]))
setTotal= preprocessor.getSets.getSet("total")
elems= setTotal.getElements
for e in elems:
crdTransf= e.getCoordTransf
#print "vector I:",crdTransf.getIVector
vILocal= crdTransf.getVectorLocalCoordFromGlobal(crdTransf.getIVector)
A = b * h # Cross section area en m2
I = 1 / 12.0 * b * h**3 # Momento de inercia en m4
theta = math.radians(30)
E = 2.0E11 # Elastic modulus en N/m2
dens = 7800 # Densidad of the steel en kg/m3
m = A * dens
NumDiv = 10
# Problem type
prueba = xc.ProblemaEF()
preprocessor = prueba.getPreprocessor
nodes = preprocessor.getNodeLoader
modelSpace = predefined_spaces.StructuralMechanics2D(nodes)
# Define materials
scc = typical_materials.defElasticSection2d(preprocessor, "scc", A, E, I)
nodes.newSeedNode()
# Geometric transformation(s)
trfs = preprocessor.getTransfCooLoader
lin = trfs.newLinearCrdTransf2d("lin")
# Definimos elemento semilla
seedElemLoader = preprocessor.getElementLoader.seedElemLoader
seedElemLoader.defaultMaterial = "scc"
seedElemLoader.defaultTransformation = "lin"
seedElemLoader.defaultTag = 1 #Number for the next element will be 1.
beam2d = seedElemLoader.newElement("elastic_beam_2d", xc.ID([0, 0]))
beam2d.h = h
beam2d.rho = m
sectionTestMaterial= typical_materials.MaterialData("sectionTestMaterial",E=7E9,nu=0.3,rho=2500) # Section material.
# Problem type
modelSpace= predefined_spaces.StructuralMechanics2D(nodes)
# Definimos el material
defSeccAggregation.defSeccAggregation2d(preprocessor, sectionTest,sectionTestMaterial)
nodes.defaultTag= 1 #First node number.
nod= nodes.newNodeXY(0,0)
nod= nodes.newNodeXY(L,0.0)
# Geometric transformations
lin= modelSpace.newLinearCrdTransf("lin")
# Materials definition
scc= typical_materials.defElasticSection2d(preprocessor, "scc",sectionTest.A(),sectionTestMaterial.E,sectionTest.Iz())
# Elements definition
elements= preprocessor.getElementHandler
elements.defaultTransformation= "lin"
elements.defaultMaterial= "scc"
elements.defaultMaterial= sectionTest.sectionName
elements.numSections= 3 # Number of sections along the element.
elements.defaultTag= 1
beam2d= elements.newElement("ForceBeamColumn2d",xc.ID([1,2]))
# Constraints
constraints= preprocessor.getBoundaryCondHandler
modelSpace.fixNode000(1)