change full_name properties to use scenario-name not scenario.name

examples/framework/tacs_oneway_naca_wing/1_tacs_sizing_opt.py

@@ -32,6 +32,9 @@
 tacs_aim = tacs_model.tacs_aim
 
 aluminum = caps2tacs.Isotropic.aluminum().register_to(tacs_model)
+aluminum_stringer = caps2tacs.Orthotropic.smeared_stringer(
+    aluminum, area_ratio=0.5
+).register_to(tacs_model)
 
 # setup the thickness design variables + automatic shell properties
 # using Composite functions, this part has to go after all funtofem variables are defined...
@@ -43,7 +46,7 @@
 for irib in range(1, nribs + 1):
     name = f"rib{irib}"
     caps2tacs.ShellProperty(
-        caps_group=name, material=aluminum, membrane_thickness=init_thickness
+        caps_group=name, material=aluminum_stringer, membrane_thickness=init_thickness
     ).register_to(tacs_model)
     Variable.structural(name, value=init_thickness).set_bounds(
         lower=0.01, upper=0.2, scale=100.0
@@ -52,7 +55,7 @@
 for ispar in range(1, nspars + 1):
     name = f"spar{ispar}"
     caps2tacs.ShellProperty(
-        caps_group=name, material=aluminum, membrane_thickness=init_thickness
+        caps_group=name, material=aluminum_stringer, membrane_thickness=init_thickness
     ).register_to(tacs_model)
     Variable.structural(name, value=init_thickness).set_bounds(
         lower=0.01, upper=0.2, scale=100.0
@@ -61,7 +64,7 @@
 for iOML in range(1, nOML + 1):
     name = f"OML{iOML}"
     caps2tacs.ShellProperty(
-        caps_group=name, material=aluminum, membrane_thickness=init_thickness
+        caps_group=name, material=aluminum_stringer, membrane_thickness=init_thickness
     ).register_to(tacs_model)
     Variable.structural(name, value=init_thickness).set_bounds(
         lower=0.01, upper=0.2, scale=100.0
@@ -149,12 +152,15 @@
 prob = om.Problem()
 
 # Create the OpenMDAO component using the built-in Funtofem component
-f2f_subsystem = FuntofemComponent(driver=tacs_driver, write_dir=tacs_aim.analysis_dir)
+design_out_file = "design-stringer.txt"
+f2f_subsystem = FuntofemComponent(
+    driver=tacs_driver, write_dir=tacs_aim.analysis_dir, design_out_file=design_out_file
+)
 prob.model.add_subsystem("f2fSystem", f2f_subsystem)
 f2f_subsystem.register_to_model(prob.model, "f2fSystem")
 
 # setup the optimizer settings # COBYLA for auto-FDing
-optimizer = "pyoptsparse"
+optimizer = "scipy"
 if optimizer == "scipy":
     prob.driver = om.ScipyOptimizeDriver(optimizer="SLSQP", tol=1.0e-9, disp=True)
 elif optimizer == "pyoptsparse":

funtofem/model/function.py

@@ -130,7 +130,7 @@ def __init__(
 
     @property
     def full_name(self) -> str:
-        return f"{self._scenario_name}.{self.name}"
+        return f"{self._scenario_name}-{self.name}"
 
     def zero_derivatives(self):
         """

funtofem/model/variable.py

@@ -138,7 +138,7 @@ def full_name(self) -> str:
         if self._scenario_name is None:
             return self.name
         else:
-            return f"{self._scenario_name}.{self.name}"
+            return f"{self._scenario_name}-{self.name}"
 
     @classmethod
     def structural(cls, name: str, value=0.0):