remove a few vals

OpenMDAO · Jan 10, 2025 · 225f641 · 225f641
1 parent e8616ad
commit 225f641
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Showing 3 changed files with 6 additions and 6 deletions.
diff --git a/aviary/subsystems/mass/gasp_based/design_load.py b/aviary/subsystems/mass/gasp_based/design_load.py
@@ -616,7 +616,7 @@ def setup(self):
         add_aviary_input(self, Aircraft.Wing.SWEEP, units="rad")
         add_aviary_input(self, Mission.Design.MACH)
 
-        add_aviary_output(self, Aircraft.Design.LIFT_CURVE_SLOPE, val=7.1765)
+        add_aviary_output(self, Aircraft.Design.LIFT_CURVE_SLOPE)
 
         self.declare_partials(Aircraft.Design.LIFT_CURVE_SLOPE, "*")
 

diff --git a/aviary/subsystems/mass/gasp_based/fixed.py b/aviary/subsystems/mass/gasp_based/fixed.py
@@ -535,7 +535,7 @@ def setup(self):
         add_aviary_output(self, Aircraft.Nacelle.MASS, shape=num_engine_type)
         self.add_output('pylon_mass', units='lbm',
                         desc='WPYLON: mass of each pylon', val=np.zeros(num_engine_type))
-        add_aviary_output(self, Aircraft.Propulsion.TOTAL_ENGINE_POD_MASS, val=0)
+        add_aviary_output(self, Aircraft.Propulsion.TOTAL_ENGINE_POD_MASS)
         add_aviary_output(self, Aircraft.Engine.ADDITIONAL_MASS,
                           shape=num_engine_type)
         self.add_output("eng_comb_mass", val=0, units="lbm",

diff --git a/aviary/subsystems/mass/gasp_based/fuel.py b/aviary/subsystems/mass/gasp_based/fuel.py
@@ -337,7 +337,7 @@ class FuelAndOEMOutputs(om.ExplicitComponent):
 
     def setup(self):
 
-        add_aviary_input(self, Aircraft.Fuel.DENSITY, val=6.687, units="lbm/ft**3")
+        add_aviary_input(self, Aircraft.Fuel.DENSITY, units="lbm/ft**3")
         add_aviary_input(self, Mission.Design.GROSS_MASS)
         add_aviary_input(self, Aircraft.Propulsion.MASS)
         add_aviary_input(self, Aircraft.Controls.TOTAL_MASS)
@@ -823,10 +823,10 @@ def setup(self):
 
         self.add_input("fus_mass_full", val=4000, units="lbm",
                        desc="WX: mass of fuselage and contents, including empennage")
-        add_aviary_input(self, Aircraft.Fuselage.MASS_COEFFICIENT, val=128)
-        add_aviary_input(self, Aircraft.Fuselage.WETTED_AREA, val=4000)
+        add_aviary_input(self, Aircraft.Fuselage.MASS_COEFFICIENT)
+        add_aviary_input(self, Aircraft.Fuselage.WETTED_AREA)
         add_aviary_input(self, Aircraft.Fuselage.AVG_DIAMETER)
-        add_aviary_input(self, Aircraft.TailBoom.LENGTH, val=129.4)
+        add_aviary_input(self, Aircraft.TailBoom.LENGTH)
         self.add_input("pylon_len", val=0, units="ft",
                        desc="ELRW: length of pylon for fuselage mounted engines")
         self.add_input("min_dive_vel", val=419.75918333, units="kn",