removing commented code

suavecode · Mar 2, 2022 · 794f0bd · 794f0bd
1 parent 5972e37
commit 794f0bd
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Showing 2 changed files with 3 additions and 3 deletions.
diff --git a/trunk/SUAVE/Methods/Geometry/Two_Dimensional/Cross_Section/Airfoil/import_airfoil_polars.py b/trunk/SUAVE/Methods/Geometry/Two_Dimensional/Cross_Section/Airfoil/import_airfoil_polars.py
@@ -39,8 +39,8 @@ def  import_airfoil_polars(airfoil_polar_files):
     num_polars   = 0
     for i in range(num_airfoils): 
         n_p = len(airfoil_polar_files[i])
-        #if n_p < 3:
-            #raise AttributeError('Provide three or more airfoil polars to compute surrogate')
+        if n_p < 3:
+            raise AttributeError('Provide three or more airfoil polars to compute surrogate')
 
         num_polars = max(num_polars, n_p)       
 

diff --git a/trunk/SUAVE/Plots/Performance/Airfoil_Plots.py b/trunk/SUAVE/Plots/Performance/Airfoil_Plots.py
@@ -346,7 +346,7 @@ def plot_airfoil_aerodynamic_coefficients(airfoil_path, airfoil_polar_paths, lin
         CL_sur = a_data.lift_coefficient_surrogates
         CD_sur = a_data.drag_coefficient_surrogates
 
-        alpha   = np.linspace(-16,16,100) #np.asarray(a_data.aoa_from_polar)
+        alpha   = np.linspace(-16,16,100)
         n_alpha = len(alpha.T)
         alpha   = np.reshape(alpha,(n_airfoils,1,n_alpha))
         alpha   = np.repeat(alpha, n_Re, axis=1)