Plane stress quad model visualization¶
This model code from Plot stress distribution of a plane stress quad model
[1]:
import opstool
import openseespy.opensees as ops
import opstool.vis.plotly as opsvis
Model¶
[2]:
ops.wipe()
ops.model("basic", "-ndm", 2, "-ndf", 2)
ops.node(1, 0.0, 0.0)
ops.node(2, 0.0, 1.0)
ops.node(3, 0.0, 2.0)
ops.node(4, 0.0, 3.0)
ops.node(5, 0.0, 4.0)
ops.node(6, 1.0, 0.0)
ops.node(7, 1.0, 1.0)
ops.node(8, 1.0, 2.0)
ops.node(9, 1.0, 3.0)
ops.node(10, 1.0, 4.0)
ops.node(11, 2.0, 0.0)
ops.node(12, 2.0, 1.0)
ops.node(13, 2.0, 2.0)
ops.node(14, 2.0, 3.0)
ops.node(15, 2.0, 4.0)
ops.node(16, 3.0, 0.0)
ops.node(17, 3.0, 1.0)
ops.node(18, 3.0, 2.0)
ops.node(19, 3.0, 3.0)
ops.node(20, 3.0, 4.0)
ops.node(21, 4.0, 0.0)
ops.node(22, 4.0, 1.0)
ops.node(23, 4.0, 2.0)
ops.node(24, 4.0, 3.0)
ops.node(25, 4.0, 4.0)
ops.nDMaterial("ElasticIsotropic", 1, 1000, 0.3)
ops.element("quad", 1, 1, 6, 7, 2, 1, "PlaneStress", 1)
ops.element("quad", 2, 2, 7, 8, 3, 1, "PlaneStress", 1)
ops.element("quad", 3, 3, 8, 9, 4, 1, "PlaneStress", 1)
ops.element("quad", 4, 4, 9, 10, 5, 1, "PlaneStress", 1)
ops.element("quad", 5, 6, 11, 12, 7, 1, "PlaneStress", 1)
ops.element("quad", 6, 7, 12, 13, 8, 1, "PlaneStress", 1)
ops.element("quad", 7, 8, 13, 14, 9, 1, "PlaneStress", 1)
ops.element("quad", 8, 9, 14, 15, 10, 1, "PlaneStress", 1)
ops.element("quad", 9, 11, 16, 17, 12, 1, "PlaneStress", 1)
ops.element("quad", 10, 12, 17, 18, 13, 1, "PlaneStress", 1)
ops.element("quad", 11, 13, 18, 19, 14, 1, "PlaneStress", 1)
ops.element("quad", 12, 14, 19, 20, 15, 1, "PlaneStress", 1)
ops.element("quad", 13, 16, 21, 22, 17, 1, "PlaneStress", 1)
ops.element("quad", 14, 17, 22, 23, 18, 1, "PlaneStress", 1)
ops.element("quad", 15, 18, 23, 24, 19, 1, "PlaneStress", 1)
ops.element("quad", 16, 19, 24, 25, 20, 1, "PlaneStress", 1)
ops.fix(1, 1, 1)
ops.fix(6, 1, 1)
ops.fix(11, 1, 1)
ops.fix(16, 1, 1)
ops.fix(21, 1, 1)
ops.equalDOF(2, 22, 1, 2)
ops.equalDOF(3, 23, 1, 2)
ops.equalDOF(4, 24, 1, 2)
ops.equalDOF(5, 25, 1, 2)
[3]:
ops.timeSeries("Linear", 1)
ops.pattern("Plain", 1, 1)
ops.load(15, 0.0, -1.0)
[4]:
opsvis.set_plot_props(point_size=3)
fig = opsvis.plot_model(show_nodal_loads=True, show_ele_loads=True, show_outline=True)
fig.write_html("images/plane_plotly.html", full_html=False, include_plotlyjs="cdn")
fig.show()
Data type cannot be displayed: application/vnd.plotly.v1+json
Results visualization¶
[5]:
ops.constraints("Transformation")
ops.numberer("RCM")
ops.system("BandGeneral")
ops.test("NormDispIncr", 1.0e-8, 6, 2)
ops.algorithm("Linear")
ops.integrator("LoadControl", 0.1)
ops.analysis("Static")
[6]:
ODB = opstool.post.CreateODB(
odb_tag=1,
compute_mechanical_measures=True, # compute stress measures, strain measures, etc.
project_gauss_to_nodes="copy", # project gauss point responses to nodes, optional ["copy", "average", "extrapolate"]
)
for _ in range(10):
ops.analyze(1)
ODB.fetch_response_step()
ODB.save_response()
OPSTOOL :: All responses data with _odb_tag = 1 saved in .opstool.output/RespStepData-1.nc!
[7]:
fig = opsvis.plot_unstruct_responses(
odb_tag=1,
slides=False,
step="absMax",
ele_type="Plane",
resp_type="StressesAtNodes", # or "stressesAtGauss", "strainsAtNodes", project_gauss_to_nodes needs to be set prior
resp_dof="sigma_vm",
show_defo=True,
defo_scale="auto",
show_model=True,
)
fig.write_html("images/plane_resp_plotly.html", full_html=False, include_plotlyjs="cdn")
fig.show()
OPSTOOL :: Loading response data from .opstool.output/RespStepData-1.nc ...
Data type cannot be displayed: application/vnd.plotly.v1+json
[8]:
fig = opsvis.plot_unstruct_responses(
odb_tag=1,
slides=True,
ele_type="Plane",
resp_type="stresses", # at Gauss points, it will be averaged over the element
resp_dof="sigma_vm",
show_model=False,
show_defo=True,
defo_scale="auto",
)
fig.write_html("images/plane_resp_plotly2.html", full_html=False, include_plotlyjs="cdn")
fig.show()
OPSTOOL :: Loading response data from .opstool.output/RespStepData-1.nc ...
Data type cannot be displayed: application/vnd.plotly.v1+json