diff --git a/openconcept/aerodynamics/openaerostruct/aerostructural.py b/openconcept/aerodynamics/openaerostruct/aerostructural.py
index 34c5ed84..6ad9e5ca 100644
--- a/openconcept/aerodynamics/openaerostruct/aerostructural.py
+++ b/openconcept/aerodynamics/openaerostruct/aerostructural.py
@@ -686,7 +686,7 @@ def compute_aerodynamic_data(point):
     compute_W_wing = point[4]
 
     # Set up OpenAeroStruct problem
-    p = om.Problem()
+    p = om.Problem(reports=False)
     p.model.add_subsystem(
         "aero_analysis",
         Aerostruct(
diff --git a/openconcept/aerodynamics/openaerostruct/drag_polar.py b/openconcept/aerodynamics/openaerostruct/drag_polar.py
index 8a17abe9..eadb89c0 100644
--- a/openconcept/aerodynamics/openaerostruct/drag_polar.py
+++ b/openconcept/aerodynamics/openaerostruct/drag_polar.py
@@ -642,7 +642,7 @@ def compute_aerodynamic_data(point):
     inputs = point[3]
 
     # Set up OpenAeroStruct problem
-    p = om.Problem()
+    p = om.Problem(reports=False)
     p.model.add_subsystem(
         "aero_analysis",
         VLM(