Add WEIS Workshop Notebooks/Scripts for Model Creation

.github/workflows/CI_WEIS.yml

@@ -152,6 +152,14 @@ jobs:
         run: |
           cd examples/09_preprocessing/fatigue
           treon Fatigue_Setup.ipynb
+
+      - name: Test model creation notebooks and drivers
+        if: contains( matrix.os, 'ubuntu') && contains( github.event_name, 'pull_request')
+        run: |
+          cd examples/11_model_creation_process
+          treon 0_notebooks/chapter1.ipynb
+          treon 0_notebooks/chapter2.ipynb
+          treon 0_notebooks/chapter3.ipynb
 
       # Run parallel script calling OpenFAST
       - name: Run parallel cases

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_DISCON.IN

@@ -1,5 +1,5 @@
 ! Controller parameter input file for the IEA-15-240-RWT-Monopile wind turbine
-!    - File written using ROSCO version 2.10.0 controller tuning logic on 09/16/25
+!    - File written using ROSCO version 2.10.1 controller tuning logic on 10/24/25
 
 !------- SIMULATION CONTROL ------------------------------------------------------------
 1                   ! LoggingLevel		- 0: write no debug files, 1: write standard output .dbg-file, 2: LoggingLevel 1 + ROSCO LocalVars (.dbg2) 3: LoggingLevel 2 + complete avrSWAP-array (.dbg3)

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_ElastoDyn.dat

@@ -73,6 +73,7 @@ True                   PtfmYDOF    - Platform yaw rotation DOF (flag)
 0.0                    TipMass(3)  - Tip-brake mass, blade 3 (kg) [unused for 2 blades]
 69131                  HubMass     - Hub mass (kg)
 969952                 HubIner     - Hub inertia about rotor axis [3 blades] or teeter axis [2 blades] (kg m^2)
+0                      HubIner_Teeter - Hub inertia about teeter axis (2-blades) (kg m^2)
 1836784                GenIner     - Generator inertia about HSS (kg m^2)
 644857                 NacMass     - Nacelle mass (kg)
 32929058               NacYIner    - Nacelle inertia about yaw axis (kg m^2)

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-Monopile/IEA-15-240-RWT-Monopile_ServoDyn.dat

@@ -74,7 +74,7 @@ True                   GenTiStp    - Method to stop the generator {T: timed usin
 ---------------------- CABLE CONTROL ---------------------------------------- 
 0                      CCmode      - Cable control mode {0- none, 4- user-defined from Simulink/Labview, 5- user-defineAfC_phased from Bladed-style DLL}
 ---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface]
-"/usr/share/miniconda3/envs/test/lib/libdiscon.so"  DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
+"/home/runner/miniconda3/envs/test/lib/libdiscon.so"  DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
 "IEA-15-240-RWT-Monopile_DISCON.IN"   DLL_InFile  - Name of input file sent to the DLL (-) [used only with Bladed Interface]
 "DISCON"               DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface]
 "default"              DLL_DT      - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface]

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi.fst

@@ -32,9 +32,9 @@ False                  Echo        - Echo input data to <RootName>.ech (flag)
 0                      MSL2SWL     - Offset between still-water level and mean sea level (m) [positive upward]
 ---------------------- INPUT FILES --------------------------------------------- 
 "IEA-15-240-RWT-UMaineSemi_ElastoDyn.dat"    EDFile          - Name of file containing ElastoDyn input parameters (quoted string) 
-"../IEA-15-240-RWT/IEA-15-240-RWT_BeamDyn.dat"   BDBldFile(1) - Name of file containing BeamDyn input parameters for blade 1 (quoted string) 
-"../IEA-15-240-RWT/IEA-15-240-RWT_BeamDyn.dat"   BDBldFile(2) - Name of file containing BeamDyn input parameters for blade 2 (quoted string) 
-"../IEA-15-240-RWT/IEA-15-240-RWT_BeamDyn.dat"   BDBldFile(3) - Name of file containing BeamDyn input parameters for blade 3 (quoted string) 
+""                     BDBldFile(1) - Name of file containing BeamDyn input parameters for blade 1 (quoted string) 
+""                     BDBldFile(2) - Name of file containing BeamDyn input parameters for blade 2 (quoted string) 
+""                     BDBldFile(3) - Name of file containing BeamDyn input parameters for blade 3 (quoted string) 
 "../IEA-15-240-RWT/IEA-15-240-RWT_InflowFile.dat"    InflowFile      - Name of file containing inflow wind input parameters (quoted string) 
 "IEA-15-240-RWT-UMaineSemi_AeroDyn15.dat"  AeroFile     - Name of file containing aerodynamic input parameters (quoted string) 
 "IEA-15-240-RWT-UMaineSemi_ServoDyn.dat"    ServoFile       - Name of file containing control and electrical-drive input parameters (quoted string) 

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi_DISCON.IN

@@ -1,5 +1,5 @@
 ! Controller parameter input file for the IEA-15-240-RWT-UMaineSemi wind turbine
-!    - File written using ROSCO version 2.10.0 controller tuning logic on 09/16/25
+!    - File written using ROSCO version 2.10.1 controller tuning logic on 10/24/25
 
 !------- SIMULATION CONTROL ------------------------------------------------------------
 1                   ! LoggingLevel		- 0: write no debug files, 1: write standard output .dbg-file, 2: LoggingLevel 1 + ROSCO LocalVars (.dbg2) 3: LoggingLevel 2 + complete avrSWAP-array (.dbg3)

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi_ElastoDyn.dat

@@ -73,6 +73,7 @@ True          PtfmYDOF    - Platform yaw rotation DOF (flag)
           0   TipMass(3)  - Tip-brake mass, blade 3 (kg) [unused for 2 blades]
       69131   HubMass     - Hub mass (kg)
      969952   HubIner     - Hub inertia about rotor axis [3 blades] or teeter axis [2 blades] (kg m^2)
+          0   HubIner_Teeter - Hub inertia about teeter axis (2-blades) (kg m^2)
     1836784   GenIner     - Generator inertia about HSS (kg m^2)
      644857   NacMass     - Nacelle mass (kg)
    32929058   NacYIner    - Nacelle inertia about yaw axis (kg m^2)

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi_HydroDyn.dat

@@ -124,4 +124,22 @@ False            OutAll         - Output all user-specified member and joint loa
 "ES11.4e2"       OutFmt         - Output format for numerical results (quoted string) [not checked for validity!]
 "A11"            OutSFmt        - Output format for header strings (quoted string) [not checked for validity!]
 ---------------------- OUTPUT CHANNELS -----------------------------------------
+"B1WvsFxi"
+"B1WvsFyi"
+"B1WvsFzi"
+"B1WvsMxi"
+"B1WvsMyi"
+"B1WvsMzi"
+"B1WvsF1xi"
+"B1WvsF1yi"
+"B1WvsF1zi"
+"B1WvsM1xi"
+"B1WvsM1yi"
+"B1WvsM1zi"
+"B1WvsF2xi"
+"B1WvsF2yi"
+"B1WvsF2zi"
+"B1WvsM2xi"
+"B1WvsM2yi"
+"B1WvsM2zi"
 END of output channels and end of file. (the word "END" must appear in the first 3 columns of this line)   

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi_SeaState.dat

@@ -69,16 +69,4 @@ False            SeaStSum       - Output a summary file [flag]
            -10,           -15    WaveKinzi - List of zi-coordinates for points where the wave kinematics can be output (meters) [NWaveKin points, separated by commas or white space; usused if NWaveKin = 0]
 ---------------------- OUTPUT CHANNELS -----------------------------------------
 "Wave1Elev"               - Wave elevation at the platform reference point (  0,  0)
-"WavesF1xi" 
-"WavesF1zi" 
-"WavesM1yi" 
-"WavesF2xi" 
-"WavesF2zi" 
-"WavesM2yi"      
-"WavesF2xi"
-"WavesF2yi"
-"WavesF2zi"
-"WavesM2xi"
-"WavesM2yi"
-"WavesM2zi" 
 END of output channels and end of file. (the word "END" must appear in the first 3 columns of this line)   

examples/00_setup/OpenFAST_models/IEA-15-240-RWT/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi_ServoDyn.dat

@@ -74,7 +74,7 @@ True                   GenTiStp    - Method to stop the generator {T: timed usin
 ---------------------- CABLE CONTROL -------------------------------------------
 0                      CCmode      - Cable control mode {0: none, 4: user-defined from Simulink/Labview, 5: user-defined from Bladed-style DLL} (switch)
 ---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface]
-"/usr/share/miniconda3/envs/test/lib/libdiscon.so"  DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
+"/home/runner/miniconda3/envs/test/lib/libdiscon.so"  DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
 "IEA-15-240-RWT-UMaineSemi_DISCON.IN"   DLL_InFile  - Name of input file sent to the DLL (-) [used only with Bladed Interface]
 "DISCON"               DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface]
 "default"              DLL_DT      - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface]

examples/02_generate_openfast_model_for_dlcs/iea34_driver.py

@@ -16,48 +16,48 @@
                                                  test_run=TEST_RUN
                                                  )
 
-
-import matplotlib.pyplot as plt
-import numpy as np
-from matplotlib import cm
-
-X = wt_opt['sse_tune.aeroperf_tables.pitch_vector']
-Y = wt_opt['sse_tune.aeroperf_tables.tsr_vector']
-X, Y = np.meshgrid(X, Y)
-pitch_schedule = wt_opt['rotorse.rp.powercurve.pitch']
-tsr_schedule = wt_opt['rotorse.rp.powercurve.Omega'] / 30. * np.pi * wt_opt['rotorse.Rtip'] / wt_opt['rotorse.rp.powercurve.V']
-
-# Plot the Cp surface
-fig, ax = plt.subplots()
-Z = wt_opt['sse_tune.aeroperf_tables.Cp']
-cs = ax.contourf(X, Y, Z[:,:,0], cmap=cm.inferno, levels = [0, 0.1, 0.2, 0.3, 0.4, 0.44, 0.47, 0.50, 0.53, 0.56])
-ax.plot(pitch_schedule, tsr_schedule, 'w--', label = 'Regulation trajectory')
-ax.set_xlabel('Pitch angle (deg)', fontweight = 'bold')
-ax.set_ylabel('Tip speed ratio (-)', fontweight = 'bold')
-cbar = fig.colorbar(cs)
-cbar.ax.set_ylabel('Aerodynamic power coefficient (-)', fontweight = 'bold')
-plt.legend()
-
-# Plot the Ct surface
-fig, ax = plt.subplots()
-Z = wt_opt['sse_tune.aeroperf_tables.Ct']
-cs = ax.contourf(X, Y, Z[:,:,0], cmap=cm.inferno)
-ax.plot(pitch_schedule, tsr_schedule, 'w--', label = 'Regulation trajectory')
-ax.set_xlabel('Pitch angle (deg)', fontweight = 'bold')
-ax.set_ylabel('Tip speed ratio (-)', fontweight = 'bold')
-cbar = fig.colorbar(cs)
-cbar.ax.set_ylabel('Aerodynamic thrust coefficient (-)', fontweight = 'bold')
-plt.legend()
-
-# Plot the Cq surface
-fig, ax = plt.subplots()
-Z = wt_opt['sse_tune.aeroperf_tables.Cq']
-cs = ax.contourf(X, Y, Z[:,:,0], cmap=cm.inferno)
-ax.plot(pitch_schedule, tsr_schedule, 'w--', label = 'Regulation trajectory')
-ax.set_xlabel('Pitch angle (deg)', fontweight = 'bold')
-ax.set_ylabel('Tip speed ratio (-)', fontweight = 'bold')
-cbar = fig.colorbar(cs)
-cbar.ax.set_ylabel('Aerodynamic torque coefficient (-)', fontweight = 'bold')
-plt.legend()
-
-plt.show()
+if not TEST_RUN:
+    import matplotlib.pyplot as plt
+    import numpy as np
+    from matplotlib import cm
+
+    X = wt_opt['sse_tune.aeroperf_tables.pitch_vector']
+    Y = wt_opt['sse_tune.aeroperf_tables.tsr_vector']
+    X, Y = np.meshgrid(X, Y)
+    pitch_schedule = wt_opt['rotorse.rp.powercurve.pitch']
+    tsr_schedule = wt_opt['rotorse.rp.powercurve.Omega'] / 30. * np.pi * wt_opt['rotorse.Rtip'] / wt_opt['rotorse.rp.powercurve.V']
+
+    # Plot the Cp surface
+    fig, ax = plt.subplots()
+    Z = wt_opt['sse_tune.aeroperf_tables.Cp']
+    cs = ax.contourf(X, Y, Z[:,:,0], cmap=cm.inferno, levels = [0, 0.1, 0.2, 0.3, 0.4, 0.44, 0.47, 0.50, 0.53, 0.56])
+    ax.plot(pitch_schedule, tsr_schedule, 'w--', label = 'Regulation trajectory')
+    ax.set_xlabel('Pitch angle (deg)', fontweight = 'bold')
+    ax.set_ylabel('Tip speed ratio (-)', fontweight = 'bold')
+    cbar = fig.colorbar(cs)
+    cbar.ax.set_ylabel('Aerodynamic power coefficient (-)', fontweight = 'bold')
+    plt.legend()
+
+    # Plot the Ct surface
+    fig, ax = plt.subplots()
+    Z = wt_opt['sse_tune.aeroperf_tables.Ct']
+    cs = ax.contourf(X, Y, Z[:,:,0], cmap=cm.inferno)
+    ax.plot(pitch_schedule, tsr_schedule, 'w--', label = 'Regulation trajectory')
+    ax.set_xlabel('Pitch angle (deg)', fontweight = 'bold')
+    ax.set_ylabel('Tip speed ratio (-)', fontweight = 'bold')
+    cbar = fig.colorbar(cs)
+    cbar.ax.set_ylabel('Aerodynamic thrust coefficient (-)', fontweight = 'bold')
+    plt.legend()
+
+    # Plot the Cq surface
+    fig, ax = plt.subplots()
+    Z = wt_opt['sse_tune.aeroperf_tables.Cq']
+    cs = ax.contourf(X, Y, Z[:,:,0], cmap=cm.inferno)
+    ax.plot(pitch_schedule, tsr_schedule, 'w--', label = 'Regulation trajectory')
+    ax.set_xlabel('Pitch angle (deg)', fontweight = 'bold')
+    ax.set_ylabel('Tip speed ratio (-)', fontweight = 'bold')
+    cbar = fig.colorbar(cs)
+    cbar.ax.set_ylabel('Aerodynamic torque coefficient (-)', fontweight = 'bold')
+    plt.legend()
+
+    plt.show()

examples/04_frequency_domain_analysis_design/iea22_raft_opt_analysis.yaml

@@ -113,8 +113,8 @@ constraints:
             flag: False
             max: 1.25  # Same as IEA-15MW with same DLCs
         nacelle_acceleration:
-            flag: False
-            max: 0.4
+            flag: True
+            max: 2.0
 
 merit_figure: structural_mass
 

examples/06_parametric_analysis/openfast_doe_driver.py

@@ -13,7 +13,7 @@
 import os
 from weis import weis_main
 
-TEST_RUN = False  # Not yet compatible with MPI
+TEST_RUN = False  # Set to True for quick testing 
 
 ## File management
 run_dir                = os.path.dirname( os.path.realpath(__file__) ) + os.sep
@@ -24,4 +24,5 @@
 wt_opt, modeling_options, opt_options = weis_main(fname_wt_input,
                                                   fname_modeling_options,
                                                   fname_analysis_options,
+                                                  test_run=TEST_RUN,
                                                   )