code/20.py

# Parameters configuration
import openseespy.opensees as ops  # Import OpenSeesPy for structural analysis
import opsvis as opsv  # Import opsvis for visualization
import matplotlib.pyplot as plt  # Import Matplotlib for plotting

ops.wipe()  # Clear any existing model
ops.model('basic', '-ndm', 2, '-ndf', 3)  # Define a 2D model with 3 degrees of freedom per node (DOF)

# Column and girder lengths
colL, girL = 4.0, 6.0

# Section properties: cross-sectional area (A) and moment of inertia (Iz)
Acol, Agir = 2.0e-3, 6.0e-3
IzCol, IzGir = 1.6e-5, 5.4e-5

# Young's modulus (E)
E = 2.0e11
# Define the material property dictionary for columns, girders, and cantilever beams
Ep = {
    1: [E, Acol, IzCol],  # Column element 1
    2: [E, Acol, IzCol],  # Column element 2
    3: [E, Agir, IzGir],  # Girder element
    4: [E, Agir, IzGir],  # Left cantilever beam
    5: [E, Agir, IzGir]   # Right cantilever beam
}

# Define the node coordinates
ops.node(1, 0, 0)          # Node 1 at (0, 0)
ops.node(2, 0, colL)        # Node 2 at (0, colL)
ops.node(3, girL, 0)        # Node 3 at (girL, 0)
ops.node(4, girL, colL)     # Node 4 at (girL, colL)
ops.node(5, -colL, colL)    # Node 5 at (-colL, colL) for left cantilever
ops.node(6, girL + colL, colL)  # Node 6 at (girL + colL, colL) for right cantilever

# Define boundary conditions (supports)
ops.fix(1, 1, 1, 1)  # Fix all 3 DOFs (x, y, rotation) for node 1
ops.fix(3, 1, 1, 1)  # Fix all 3 DOFs (x, y, rotation) for node 3

# Plot the model before defining elements
opsv.plot_model()
# Add title
plt.title('plot_model before defining elements')

# Define transformation type for elements (Linear)
ops.geomTransf('Linear', 1)  # Transformation ID 1 for linear transformation

# Define column and girder elements (elastic beam-column elements)
ops.element('elasticBeamColumn', 1, 1, 2, Acol, E, IzCol, 1)  # Column element 1 between nodes 1 and 2
ops.element('elasticBeamColumn', 2, 3, 4, Acol, E, IzCol, 1)  # Column element 2 between nodes 3 and 4
ops.element('elasticBeamColumn', 3, 2, 4, Agir, E, IzGir, 1)  # Girder element between nodes 2 and 4
ops.element('elasticBeamColumn', 4, 5, 2, Agir, E, IzGir, 1)  # Left cantilever beam between nodes 5 and 2
ops.element('elasticBeamColumn', 5, 4, 6, Agir, E, IzGir, 1)  # Right cantilever beam between nodes 4 and 6

# Define external loads
Wy = -10e3  # Uniformly distributed load in the y-direction

# Create a dictionary to store element loads
Ew = {
    3: ['-beamUniform', Wy, 0],  # Girder element has a uniform distributed load
    4: ['-beamUniform', Wy, 0],  # Left cantilever beam has a uniform distributed load
    5: ['-beamUniform', Wy, 0]   # Right cantilever beam has a uniform distributed load
}

# Define time series for constant loads
ops.timeSeries('Constant', 1)
# Define load pattern using the constant time series
ops.pattern('Plain', 1, 1)

# Applying distributed loads
for etag in Ew:
    ops.eleLoad('-ele', etag, '-type', Ew[etag][0], Ew[etag][1], Ew[etag][2])
# Analysis settings
ops.constraints('Transformation')  # Apply transformation constraints
ops.numberer('RCM')  # Renumber the nodes using Reverse Cuthill-McKee (RCM)
ops.system('BandGeneral')  # Define the solution algorithm
ops.test('NormDispIncr', 1.0e-6, 6, 2)  # Convergence test criteria
ops.algorithm('Linear')  # Use linear algorithm for solving
ops.integrator('LoadControl', 1)  # Control load increments
ops.analysis('Static')  # Define a static analysis
ops.analyze(1)  # Perform the analysis

# Print the model data
ops.printModel()

# Plot the model after defining elements
opsv.plot_model()
plt.title('plot_model after defining elements')

# Plot the applied loads on the model in 2D
opsv.plot_loads_2d(nep=10,  # Number of points along each element
                   sfac=1,  # Scale factor for loads
                   fig_wi_he=(10, 5),  # Width and height of the figure
                   fig_lbrt=(0.1, 0.1, 0.9, 0.9),  # Left, bottom, right, top margins
                   fmt_model_loads={'color': 'red', 'linewidth': 1.5},  # Formatting for load arrows
                   node_supports=True,  # Display node supports
                   truss_node_offset=0.05,  # Offset for truss elements
                   ax=None)  # Matplotlib axis, None to use current axis

# Plot deformations (scaled) after analysis
opsv.plot_defo()

# Plot internal force diagrams: N (axial), V (shear), M (moment)
sfacN, sfacV, sfacM = 5.e-5, 5.e-5, 5.e-5  # Scale factors for internal force diagrams

# Plot axial force distribution
opsv.section_force_diagram_2d('N', sfacN)
plt.title('Axial force distribution')

# Plot shear force distribution
opsv.section_force_diagram_2d('T', sfacV)
plt.title('Shear force distribution')

# Plot bending moment distribution
opsv.section_force_diagram_2d('M', sfacM)
plt.title('Bending moment distribution')

# Show all plots
plt.show()

# Exit the program
exit()