code/18.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, girder, and brace dimensions
colL, girL, braceL = 4e0, 6e0, 4e0

# Section properties: cross-sectional area (A) and moment of inertia (Iz)
Acol, Agir, Abr = 2e-3, 6e-3, 6e-3
IzCol, IzGir, IzBr = 1.6e-5, 5.4e-5, 5.4e-5

# Young's modulus (E)
E = 2e11

# Uniform distributed load on the girder (N/m)
qGir = 1e4
# Define the material property dictionary for columns and girders
Ep = {
    1: [2e11, 2e-3, 1.6e-5],  # Column elements
    2: [2e11, 6e-3, 5.4e-5],  # Girder element
    3: [2e11, 6e-3, 5.4e-5]   # Diagonal elements
}

# Define the node coordinates
ops.node(1, 0, 0)          # Bottom left support
ops.node(2, 0, 4.0)        # Top of the left column
ops.node(3, 6.0, 0)        # Bottom right support
ops.node(4, 6.0, 4.0)      # Top of the right column
ops.node(5, -4.0, 0)       # Ground connection of left diagonal brace
ops.node(6, 10.0, 0)       # Ground connection of right diagonal brace

# Define boundary conditions (supports)
ops.fix(1, 1, 1, 1)  # Fix all DOFs for node 1
ops.fix(3, 1, 1, 1)  # Fix all DOFs for node 3
ops.fix(5, 1, 1, 1)  # Fix all DOFs for the bottom left diagonal node
ops.fix(6, 1, 1, 1)  # Fix all DOFs for the bottom right diagonal node

# 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)

# Define column and girder elements (elastic beam-column elements)
ops.element('elasticBeamColumn', 1, 1, 2, 2e-3, 2e11, 1.6e-5, 1)  # Left column
ops.element('elasticBeamColumn', 2, 2, 4, 6e-3, 2e11, 5.4e-5, 1)  # Girder
ops.element('elasticBeamColumn', 3, 4, 3, 2e-3, 2e11, 1.6e-5, 1)  # Right column
ops.element('elasticBeamColumn', 4, 2, 5, 6e-3, 2e11, 5.4e-5, 1)  # Left diagonal brace
ops.element('elasticBeamColumn', 5, 4, 6, 6e-3, 2e11, 5.4e-5, 1)  # Right diagonal brace

# Define external loads
Wy = -1e4  # Uniform distributed load in the y-direction
Wx = 0     # No horizontal distributed load

# Create a dictionary to store element loads
Ew = {
    2: ['-beamUniform', Wy, Wx]  # Distributed load on girder element 2
}

# Define time series for constant loads
ops.timeSeries('Constant', 1)

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

# Applying point loads
# No point loads to apply in this case

# 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()