set val in two places

OpenMDAO · Jan 11, 2025 · 3b083fb · 3b083fb
1 parent 159b81c
commit 3b083fb
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Showing 2 changed files with 2 additions and 2 deletions.
diff --git a/aviary/subsystems/geometry/gasp_based/empennage.py b/aviary/subsystems/geometry/gasp_based/empennage.py
@@ -104,7 +104,7 @@ def setup(self):
                            "For a horizontal tail, the mean wing chord. For a "
                            "vertical tail, the wing span.")
                        )
-        self.add_input("ar", 4.75, units="unitless",
+        self.add_input("ar", 0.0, units="unitless",
                        desc="ARHT | ARVT: Tail aspect ratio.")
         self.add_input("tr", 0.352, units="unitless",
                        desc="SLMH | SLMV: Tail taper ratio.")

diff --git a/aviary/subsystems/geometry/gasp_based/wing.py b/aviary/subsystems/geometry/gasp_based/wing.py
@@ -542,7 +542,7 @@ def setup(self):
         add_aviary_input(self, Aircraft.Wing.TAPER_RATIO)
         add_aviary_input(self, Aircraft.Wing.THICKNESS_TO_CHORD_ROOT)
         add_aviary_input(self, Aircraft.Wing.THICKNESS_TO_CHORD_TIP)
-        add_aviary_input(self, Aircraft.Fuel.WING_FUEL_FRACTION, val=0.6)
+        add_aviary_input(self, Aircraft.Fuel.WING_FUEL_FRACTION)
 
         self.add_output("nonfolded_taper_ratio", val=0.1, units="unitless",
                         desc="SLM_NF: taper ratio between wing root and fold location",