Merge pull request #3 from nasa/1.0.5-bug-fixes-troubleshoopting

1.0.5 bug fixes troubleshoopting
nasa · Jul 8, 2023 · 3c7ae26 · 3c7ae26
2 parents dcdb04a + 4526d4e
commit 3c7ae26
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diff --git a/.gitignore b/.gitignore
@@ -190,3 +190,6 @@ tgs_format.py
 *.q
 *.soln
 .DS_Store
+
+# folders 
+solidwork_curves.txt/
diff --git a/pyproject.toml b/pyproject.toml
@@ -1,6 +1,6 @@
 [tool.poetry]
 name = "pyturbo-aero"
-version = "1.0.4"
+version = "1.0.5"
 description = "PyTurbo_Aero is a Turbomachinery blade design library that lets you create a full 3D blades and passages."
 authors = ["Paht Juangphanich <[email protected]>"]
 packages = [

diff --git a/pyturbo/aero/airfoil2D.py b/pyturbo/aero/airfoil2D.py
@@ -772,14 +772,14 @@ def plot2D(self):
             x = self.ssBezierX[indx]
             y = self.ssBezierY[indx]
             d = dist(x,y,xcamber,ycamber)
-            min_indx = np.where(d == np.amin(d))
+            min_indx = np.where(d == np.amin(d))[0][0]
             plt.plot([x,xcamber[min_indx]],[y,ycamber[min_indx]], color='black', linestyle='dashed')
         # pressure side
         for indx in range(0,len(self.psBezierX)):
             x = self.psBezierX[indx]
             y = self.psBezierY[indx]
             d = dist(x,y,xcamber,ycamber)
-            min_indx = np.where(d == np.amin(d))
+            min_indx = np.where(d == np.amin(d))[0][0]
             plt.plot([x,xcamber[min_indx]],[y,ycamber[min_indx]], color='black', linestyle='dashed')
         # Plot the Trailing Edge
         t = np.linspace(0,1,20)

diff --git a/tutorials/2D_DesignTutorial.ipynb b/tutorials/2D_DesignTutorial.ipynb
diff --git a/tutorials/3D_DesignTutorial.ipynb b/tutorials/3D_DesignTutorial.ipynb
diff --git a/tutorials/3D_design_test.py b/tutorials/3D_design_test.py
@@ -17,7 +17,7 @@
 stator_hub.te_create(radius=0.001,wedge_ss=2.5,wedge_ps=2.4)
 
 stator_hub.flow_guidance2(10)
-
+stator_hub.plot2D()
 stator_mid = airfoil2D(alpha1=10,alpha2=72,axial_chord=0.038,stagger=45) # This creates the camberline
 # Building Leading Edge
 stator_mid.le_thickness_add(0.06)

diff --git a/tutorials/blade.stl b/tutorials/blade.stl