Source code for tacs.mphys.builder

-import copy
-import warnings
-
-from mphys.builder import Builder
+from mphys.core import Builder, MPhysVariables
 import numpy as np
 
 from tacs.pytacs import pyTACS
@@ -62,7 +59,7 @@ 
Source code for tacs.mphys.builder
         pytacs_options=None,
         check_partials=False,
         conduction=False,
-        coupled=True,
+        coupling_loads=None,
         write_solution=True,
         separate_mass_dvs=False,
         res_ref=None,
@@ -141,9 +138,10 @@ 
Source code for tacs.mphys.builder
         conduction : bool, optional
             Flag to determine weather TACS component represents a thermal (True) or structural (False) analysis.
             Defaults to False.
-        coupled : bool, optional
-            Flag to determine of if multidisciplinary coupling variables should be turned on
-            (used in aerostructural/thermostructural analyses). Defaults to True.
+        coupling_loads : list[str] or str or None, optional
+            List of coupling loads to add to right handside of FEA state equation. These loads correspond to the nodal
+            forces on the model. Multiple load sources can be specified, these will be added together before being
+            applied to the model. This is used in aerostructural/thermostructural analyses. Defaults to None.
         write_solution : bool, optional
             Flag to determine whether to write out TACS solutions to f5 file each design iteration. Defaults to True.
         separate_mass_dvs : bool, optional
@@ -243,7 +241,12 @@ 
Source code for tacs.mphys.builder
         self.pytacs_options = pytacs_options
         self.check_partials = check_partials
         self.conduction = conduction
-        self.coupled = coupled
+        if isinstance(coupling_loads, str):
+            self.coupling_loads = [coupling_loads]
+        elif hasattr(coupling_loads, "__iter__"):
+            self.coupling_loads = coupling_loads
+        else:
+            self.coupling_loads = []
         self.write_solution = write_solution
         self.separate_mass_dvs = separate_mass_dvs
         self.res_ref = res_ref
@@ -271,7 +274,14 @@ 
Source code for tacs.mphys.builder
             self.assembler_setup(self.fea_assembler)
 
         # Set up elements and TACS assembler
-        self.fea_assembler.initialize(self.element_callback)

+        self.fea_assembler.initialize(self.element_callback)
+
+        if self.conduction:
+            self.discipline_vars = MPhysVariables.Thermal
+            self.discipline_vars.STATES = self.discipline_vars.TEMPERATURE
+        else:
+            self.discipline_vars = MPhysVariables.Structures
+            self.discipline_vars.STATES = self.discipline_vars.DISPLACEMENTS

 
 
 

@@ -293,9 +303,9 @@ 
Source code for tacs.mphys.builder
         """
         return TacsCouplingGroup(
             fea_assembler=self.fea_assembler,
-            conduction=self.conduction,
+            discipline_vars=self.discipline_vars,
             check_partials=self.check_partials,
-            coupled=self.coupled,
+            coupling_loads=self.coupling_loads,
             scenario_name=scenario_name,
             problem_setup=self.problem_setup,
             res_ref=self.res_ref,
@@ -319,7 +329,10 @@ 
Source code for tacs.mphys.builder
         mesh : :class:`~openmdao.api.Component` or :class:`~openmdao.api.Group`
             The openmdao subsystem that has an output of coordinates.
         """
-        return TacsMeshGroup(fea_assembler=self.fea_assembler)

+        return TacsMeshGroup(
+            fea_assembler=self.fea_assembler,
+            discipline_vars=self.discipline_vars,
+        )

 
 
 

@@ -342,6 +355,7 @@ 
Source code for tacs.mphys.builder
             fea_assembler=self.fea_assembler,
             initial_dv_vals=initial_dvs,
             separate_mass_dvs=self.separate_mass_dvs,
+            discipline_vars=self.discipline_vars,
         )

 
 
@@ -363,7 +377,7 @@ 
Source code for tacs.mphys.builder
         return TacsPostcouplingGroup(
             fea_assembler=self.fea_assembler,
             check_partials=self.check_partials,
-            conduction=self.conduction,
+            discipline_vars=self.discipline_vars,
             write_solution=self.write_solution,
             scenario_name=scenario_name,
             problem_setup=self.problem_setup,
diff --git a/_sources/examples/Example-Beam_Optimization.rst.txt b/_sources/examples/Example-Beam_Optimization.rst.txt
index c9b825b70..abd243a0f 100644
--- a/_sources/examples/Example-Beam_Optimization.rst.txt
+++ b/_sources/examples/Example-Beam_Optimization.rst.txt
@@ -37,8 +37,8 @@ First, we import required libraries, define the model bdf file, and define impor
   import matplotlib.pyplot as plt
   import numpy as np
   import openmdao.api as om
-  from mphys import Multipoint
-  from mphys.scenario_structural import ScenarioStructural
+  from mphys.core import Multipoint, MPhysVariables
+  from mphys.scenarios import ScenarioStructural
 
   from tacs import elements, constitutive, functions
   from tacs.mphys import TacsBuilder
@@ -120,7 +120,6 @@ We use this builder to create an MPhys :class:`~mphys.StructuralScenario`.
               mesh_file=bdf_file,
               element_callback=element_callback,
               problem_setup=problem_setup,
-              coupled=False,
               write_solution=False,
           )
           struct_builder.initialize(self.comm)
@@ -135,7 +134,10 @@ We use this builder to create an MPhys :class:`~mphys.StructuralScenario`.
           self.mphys_add_scenario(
               "tip_shear", ScenarioStructural(struct_builder=struct_builder)
           )
-          self.mphys_connect_scenario_coordinate_source("mesh", "tip_shear", "struct")
+          self.connect(
+              f"mesh.{MPhysVariables.Structures.Mesh.COORDINATES}",
+              f"tip_shear.{MPhysVariables.Structures.COORDINATES}",
+          )
 
           # Connect dv component to input of structural scenario
           self.connect("dv_struct", "tip_shear.dv_struct")
@@ -196,7 +198,9 @@ Finally, we can plot the optimized thickness distribution using matplotlib and c
 .. code-block:: python
 
   # Get optimized solution variables
-  x = prob.get_val("mesh.x_struct0", get_remote=True)[:-3:3]
+  x = prob.get_val(f"mesh.{MPhysVariables.Structures.Mesh.COORDINATES}", get_remote=True)[
+    :-3:3
+  ]
   t_opt = prob["dv_struct"]
   m_opt = prob["tip_shear.mass"]
 
diff --git a/_sources/examples/Example-Composite_Optimization.rst.txt b/_sources/examples/Example-Composite_Optimization.rst.txt
index f92f5d1ec..61e79d992 100644
--- a/_sources/examples/Example-Composite_Optimization.rst.txt
+++ b/_sources/examples/Example-Composite_Optimization.rst.txt
@@ -34,8 +34,8 @@ To begin we first import required libraries, define the model bdf file, and defi
 
   import openmdao.api as om
   import numpy as np
-  from mphys import Multipoint
-  from mphys.scenario_structural import ScenarioStructural
+  from mphys.core import Multipoint
+from mphys.scenarios import ScenarioStructural
 
   from tacs import elements, constitutive, functions
   from tacs.mphys import TacsBuilder
@@ -168,7 +168,6 @@ We use this builder to create an MPhys :class:`~mphys.StructuralScenario`.
               element_callback=element_callback,
               problem_setup=problem_setup,
               constraint_setup=constraint_setup,
-              coupled=False,
               check_partials=True,
           )
           struct_builder.initialize(self.comm)
@@ -181,7 +180,10 @@ We use this builder to create an MPhys :class:`~mphys.StructuralScenario`.
           self.mphys_add_scenario(
               "pressure_load", ScenarioStructural(struct_builder=struct_builder)
           )
-          self.mphys_connect_scenario_coordinate_source("mesh", "pressure_load", "struct")
+        self.connect(
+            f"mesh.{MPhysVariables.Structures.Mesh.COORDINATES}",
+            f"pressure_load.{MPhysVariables.Structures.COORDINATES}",
+        )
 
           self.connect("dv_struct", "pressure_load.dv_struct")
 
diff --git a/examples/Example-Beam_Optimization.html b/examples/Example-Beam_Optimization.html
index e03233b21..2bf15c39b 100644
--- a/examples/Example-Beam_Optimization.html
+++ b/examples/Example-Beam_Optimization.html
@@ -73,8 +73,8 @@ 
Beam optimization with MPhysimport matplotlib.pyplot as plt
 import numpy as np
 import openmdao.api as om
-from mphys import Multipoint
-from mphys.scenario_structural import ScenarioStructural
+from mphys.core import Multipoint, MPhysVariables
+from mphys.scenarios import ScenarioStructural
 
 from tacs import elements, constitutive, functions
 from tacs.mphys import TacsBuilder
@@ -139,7 +139,7 @@ 
Beam optimization with MPhysproblem.addLoadToNodes(101, [0.0, V, 0.0, 0.0, 0.0, 0.0], nastranOrdering=True)
 

 

-
Here we define our Multipoint (essentially an OpenMDAO Group) which will contain our analysis Scenario.
+
Here we define our Multipoint (essentially an OpenMDAO Group) which will contain our analysis Scenario.
 To do this, we instantiate the TacsBuilder using the element_callback and problem_setup we defined above.
 We create OpenMDAO Component's to feed design variable and mesh inputs to the Scenario component.
 We use this builder to create an MPhys StructuralScenario.

@@ -150,7 +150,6 @@ 
Beam optimization with MPhysmesh_file=bdf_file,
             element_callback=element_callback,
             problem_setup=problem_setup,
-            coupled=False,
             write_solution=False,
         )
         struct_builder.initialize(self.comm)
@@ -165,7 +164,10 @@ 
Beam optimization with MPhysself.mphys_add_scenario(
             "tip_shear", ScenarioStructural(struct_builder=struct_builder)
         )
-        self.mphys_connect_scenario_coordinate_source("mesh", "tip_shear", "struct")
+        self.connect(
+            f"mesh.{MPhysVariables.Structures.Mesh.COORDINATES}",
+            f"tip_shear.{MPhysVariables.Structures.COORDINATES}",
+        )
 
         # Connect dv component to input of structural scenario
         self.connect("dv_struct", "tip_shear.dv_struct")
@@ -220,7 +222,9 @@ 
Beam optimization with MPhys
# Get optimized solution variables
-x = prob.get_val("mesh.x_struct0", get_remote=True)[:-3:3]
+x = prob.get_val(f"mesh.{MPhysVariables.Structures.Mesh.COORDINATES}", get_remote=True)[
+  :-3:3
+]
 t_opt = prob["dv_struct"]
 m_opt = prob["tip_shear.mass"]
 
diff --git a/examples/Example-Composite_Optimization.html b/examples/Example-Composite_Optimization.html
index e3ee3dc34..02aff65e7 100644
--- a/examples/Example-Composite_Optimization.html
+++ b/examples/Example-Composite_Optimization.html
@@ -73,42 +73,38 @@ 
Composite plate optimization with MPhysimport openmdao.api as om
 import numpy as np
-from mphys import Multipoint
-from mphys.scenario_structural import ScenarioStructural
-
-from tacs import elements, constitutive, functions
-from tacs.mphys import TacsBuilder
-
-# BDF file containing mesh
-bdf_file = os.path.join(os.path.dirname(__file__), "partitioned_plate.bdf")
-
-# Material properties
-rho = 1550.0
-E1 = 54e9
-E2 = 18e9
-nu12 = 0.25
-G12 = 9e9
-G13 = 9e9
-Xt = 2410.0e6
-Xc = 1040.0e6
-Yt = 73.0e6
-Yc = 173.0e6
-S12 = 71.0e6
-
-# Shell thickness
-ply_thickness = 1.25e-3  # m
-plate_thickness = 0.05  # m
-tMin = 0.002  # m
-tMax = 0.05  # m
-
-# Ply angles/initial ply fractions
-ply_angles = np.deg2rad([0.0, 45.0, -45.0, 90.0])
-ply_fractions = np.array([0.25, 0.25, 0.25, 0.25])
-
-# Pressure load to apply to plate
-P = 100e3
+from mphys.core import Multipoint
 

 

+
from mphys.scenarios import ScenarioStructural

+

+
from tacs import elements, constitutive, functions
+from tacs.mphys import TacsBuilder

+
# BDF file containing mesh
+bdf_file = os.path.join(os.path.dirname(__file__), "partitioned_plate.bdf")

+
# Material properties
+rho = 1550.0
+E1 = 54e9
+E2 = 18e9
+nu12 = 0.25
+G12 = 9e9
+G13 = 9e9
+Xt = 2410.0e6
+Xc = 1040.0e6
+Yt = 73.0e6
+Yc = 173.0e6
+S12 = 71.0e6

+
# Shell thickness
+ply_thickness = 1.25e-3  # m
+plate_thickness = 0.05  # m
+tMin = 0.002  # m
+tMax = 0.05  # m

+
# Ply angles/initial ply fractions
+ply_angles = np.deg2rad([0.0, 45.0, -45.0, 90.0])
+ply_fractions = np.array([0.25, 0.25, 0.25, 0.25])

+
# Pressure load to apply to plate
+P = 100e3

+

 
Next, we define an element_callback function for setting up the TACS elements and design variables.
 We use the SmearedCompositeShellConstitutive class here for the constitutive properties, and
 assign four design variable numbers to each element (one for each ply fraction), and return a Quad4Shell element class.

@@ -188,7 +184,7 @@ 
Composite plate optimization with MPhysconstraint_list.append(constr)
 

 

-
Fianlly, we define our Multipoint class.
+
Fianlly, we define our Multipoint class.
 To do this, we instantiate the TacsBuilder using the element_callback, problem_setup, and constraint_setup we defined above.
 We create OpenMDAO Component's to feed design variable and mesh inputs to the Scenario component.
 We use this builder to create an MPhys StructuralScenario.

@@ -199,7 +195,6 @@ 
Composite plate optimization with MPhyselement_callback=element_callback,
             problem_setup=problem_setup,
             constraint_setup=constraint_setup,
-            coupled=False,
             check_partials=True,
         )
         struct_builder.initialize(self.comm)
@@ -212,7 +207,10 @@ 
Composite plate optimization with MPhysself.mphys_add_scenario(
             "pressure_load", ScenarioStructural(struct_builder=struct_builder)
         )
-        self.mphys_connect_scenario_coordinate_source("mesh", "pressure_load", "struct")
+      self.connect(
+          f"mesh.{MPhysVariables.Structures.Mesh.COORDINATES}",
+          f"pressure_load.{MPhysVariables.Structures.COORDINATES}",
+      )
 
         self.connect("dv_struct", "pressure_load.dv_struct")
diff --git a/mphys/builder.html b/mphys/builder.html index 261515428..335ce0af4 100644 --- a/mphys/builder.html +++ b/mphys/builder.html @@ -119,8 +119,9 @@

API Referencebool, optional) -- Flag to determine weather TACS component represents a thermal (True) or structural (False) analysis. Defaults to False.

-

  • coupled (bool, optional) -- Flag to determine of if multidisciplinary coupling variables should be turned on -(used in aerostructural/thermostructural analyses). Defaults to True.

    • +

  • coupling_loads (list[str] or str or None, optional) -- List of coupling loads to add to right handside of FEA state equation. These loads correspond to the nodal +forces on the model. Multiple load sources can be specified, these will be added together before being +applied to the model. This is used in aerostructural/thermostructural analyses. Defaults to None.

  • write_solution (bool, optional) -- Flag to determine whether to write out TACS solutions to f5 file each design iteration. Defaults to True.

  • separate_mass_dvs (bool, optional) -- Flag to determine if TACS' mass dvs should be lumped into the struct_dv input vector (False) or split into separate OpenMDAO inputs based on their assigned names (True). Defaults to False.

    • diff --git a/searchindex.js b/searchindex.js index d46395be0..cc59eda3e 100644 --- a/searchindex.js +++ b/searchindex.js @@ -1 +1 @@ -Search.setIndex({"alltitles": {"API Reference": [[15, "api-reference"], [17, "api-reference"], [18, "api-reference"], [19, "api-reference"], [21, "api-reference"], [22, "api-reference"], [23, "api-reference"], [24, "api-reference"], [25, "api-reference"], [26, "api-reference"], [29, "api-reference"], [31, "api-reference"], [32, "api-reference"], [33, "api-reference"]], "AdjacencyConstraint": [[17, null]], "Assembler": [[2, "assembler"]], "BaseSolver": [[18, null]], "Basic steps to compile TACS": [[13, "basic-steps-to-compile-tacs"]], "Basis classes": [[5, "basis-classes"]], "Battery pack during thermal runaway": [[11, null]], "Beam and shell elements in TACS": [[35, null]], "Beam element implementation": [[35, "beam-element-implementation"]], "Beam optimization with MPhys": [[7, null]], "Beam volume parametrization": [[35, "beam-volume-parametrization"]], "BucklingProblem": [[19, null]], "CRM Optimization": [[8, null]], "Checking out the code": [[13, "checking-out-the-code"]], "Composite plate optimization with MPhys": [[9, null]], "Constitutive classes": [[3, "constitutive-classes"]], "Constitutive relationships for the shell element": [[35, "constitutive-relationships-for-the-shell-element"]], "Constraint classes": [[20, null]], "ContinuationSolver": [[21, null]], "Core modules": [[4, null]], "Creator": [[2, "creator"]], "DVConstraint": [[22, null]], "Detailed installation instructions": [[13, "detailed-installation-instructions"]], "Direct": [[2, null]], "Director field parametrization": [[35, "director-field-parametrization"]], "Director implementation": [[35, "director-implementation"]], "Director parametrization": [[35, "director-parametrization"]], "Displacement parametrization": [[35, "displacement-parametrization"]], "Drilling rotation": [[35, "drilling-rotation"]], "Element classes": [[5, 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