Conflict resolve

OpenMDAO · Jan 9, 2025 · 8cef416 · 8cef416
1 parent ec89f78
commit 8cef416
Showing 1 changed file with 3 additions and 11 deletions.
diff --git a/aviary/subsystems/aerodynamics/flops_based/tabular_aero_group.py b/aviary/subsystems/aerodynamics/flops_based/tabular_aero_group.py
@@ -139,11 +139,11 @@ def setup(self):
             'lift_coefficient',
             CL(num_nodes=nn),
             promotes_inputs=[
-                Dynamic.Mission.MASS,
+                Dynamic.Vehicle.MASS,
                 Aircraft.Wing.AREA,
-                Dynamic.Mission.DYNAMIC_PRESSURE,
+                Dynamic.Atmosphere.DYNAMIC_PRESSURE,
             ],
-            promotes_outputs=[('cl', 'lift_coefficient'), Dynamic.Mission.LIFT])
+            promotes_outputs=[('cl', 'lift_coefficient'), Dynamic.Vehicle.LIFT])
 
         if connect_training_data:
             extra_promotes = [('zero_lift_drag_coefficient_train',
@@ -171,14 +171,6 @@ def setup(self):
             promotes_outputs=['*'],
         )
 
-        self.add_subsystem(
-            'CD0_interp', CD0_interp, promotes_inputs=['*'], promotes_outputs=['*']
-        )
-
-        self.add_subsystem(
-            'CDI_interp', CDI_interp, promotes_inputs=['*'], promotes_outputs=['*']
-        )
-
         self.add_subsystem(
             Dynamic.Vehicle.DRAG,
             Drag(num_nodes=nn),