set Aircraft.Engine.ADDITIONAL_MASS_FRACTIO = val=np.full(num_engine_…

…type, 0.14)
OpenMDAO · Jan 9, 2025 · b96194b · b96194b
1 parent c8023de
commit b96194b
Showing 1 changed file with 1 addition and 1 deletion.
diff --git a/aviary/subsystems/mass/gasp_based/fixed.py b/aviary/subsystems/mass/gasp_based/fixed.py
@@ -514,7 +514,7 @@ def setup(self):
         add_aviary_input(self, Aircraft.Engine.PYLON_FACTOR,
                          shape=num_engine_type)
         add_aviary_input(self, Aircraft.Engine.ADDITIONAL_MASS_FRACTION,
-                         shape=num_engine_type)
+                         val=np.full(num_engine_type, 0.14))
         add_aviary_input(self, Aircraft.Engine.MASS_SCALER,
                          shape=num_engine_type)
         add_aviary_input(self, Aircraft.Propulsion.MISC_MASS_SCALER)