Updated tutorials

nasa · Mar 4, 2024 · 0ff3ea6 · 0ff3ea6
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diff --git a/tutorials/3D_DesignTutorial.ipynb b/tutorials/3D_DesignTutorial.ipynb
@@ -73,10 +73,10 @@
       "source": [
         "import sys\n",
         "import numpy as np\n",
-        "from pyturbo.aero import airfoil2D\n",
+        "from pyturbo.aero import Airfoil2D\n",
         "from pyturbo.helper import exp_ratio\n",
         "\n",
-        "stator_hub = airfoil2D(alpha1=0,alpha2=72,axial_chord=0.04,stagger=50) # This creates the camberline\n",
+        "stator_hub = Airfoil2D(alpha1=0,alpha2=72,axial_chord=0.04,stagger=50) # This creates the camberline\n",
         "# Building Leading Edge\n",
         "stator_hub.le_thickness_add(0.04)\n",
         "# Building the Pressure side \n",
@@ -122,7 +122,7 @@
         }
       ],
       "source": [
-        "stator_mid = airfoil2D(alpha1=10,alpha2=72,axial_chord=0.038,stagger=45) # This creates the camberline\n",
+        "stator_mid = Airfoil2D(alpha1=10,alpha2=72,axial_chord=0.038,stagger=45) # This creates the camberline\n",
         "# Building Leading Edge\n",
         "stator_mid.le_thickness_add(0.06)\n",
         "# Building the Pressure side \n",
@@ -168,7 +168,7 @@
         }
       ],
       "source": [
-        "stator_tip = airfoil2D(alpha1=5,alpha2=60,axial_chord=0.038,stagger=40) # This creates the camberline\n",
+        "stator_tip = Airfoil2D(alpha1=5,alpha2=60,axial_chord=0.038,stagger=40) # This creates the camberline\n",
         "# Building Leading Edge\n",
         "stator_tip.le_thickness_add(0.04)\n",
         "# Building the Pressure side \n",
@@ -241,10 +241,10 @@
         }
       ],
       "source": [
-        "from pyturbo.aero import airfoil3D, stack_type\n",
+        "from pyturbo.aero import Airfoil3D, stack_type\n",
         "import matplotlib.pyplot as plt \n",
         "\n",
-        "stator3D = airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.02)\n",
+        "stator3D = Airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.02)\n",
         "stator3D.stack(stack_type.leading_edge) # Stators are typically stacked with leading edge; rotors with centroid or trailing edge\n",
         "# You can also use stack_type.centroid or stack_type.trailing_edge\n",
         "stator3D.create_blade(20,160,20) \n",
@@ -285,7 +285,7 @@
         }
       ],
       "source": [
-        "stator3D = airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.02)\n",
+        "stator3D = Airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.02)\n",
         "stator3D.stack(stack_type.trailing_edge) # Stators are typically stacked with leading edge; rotors with centroid or trailing edge\n",
         "# You can also use stack_type.centroid or stack_type.trailing_edge\n",
         "stator3D.create_blade(20,160,20) \n",
@@ -377,7 +377,7 @@
         }
       ],
       "source": [
-        "stator3D = airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.02)\n",
+        "stator3D = Airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.02)\n",
         "stator3D.stack(stack_type.centroid)\n",
         "stator3D.lean_add(leanX=[0,0.03,0.01], leanZ=[0.0, 0.5, 1]) # Z =1 is blade tip, Z = 0 is blade hub. The units are in percentage \n",
         "stator3D.create_blade(20,160,20) \n",
@@ -414,7 +414,7 @@
         }
       ],
       "source": [
-        "stator3D = airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.04)\n",
+        "stator3D = Airfoil3D(profileArray=[stator_hub,stator_mid,stator_tip],profile_loc=[0.0,0.5,1.0], height = 0.04)\n",
         "stator3D.stack(stack_type.leading_edge) # Stators are typically stacked with leading edge; rotors with centroid or trailing edge\n",
         "stator3D.sweep(sweep_y=[0,0.5,0.2], sweep_z=[0.0, 0.5, 1]) # Z =1 is blade tip, Z = 0 is blade hub. The units are in percentage \n",
         "stator3D.create_blade(20,160,20)    \n",

diff --git a/tutorials/3D_design_test.py b/tutorials/3D_design_test.py
@@ -53,7 +53,7 @@
 stator3D.stack(stack_type.centroid) # Stators are typically stacked with leading edge; rotors with centroid or trailing edge
 stator3D.sweep(sweep_y=[0,-0.05,0.05], sweep_z=[0.0, 0.5, 1]) # Z =1 is blade tip, Z = 0 is blade hub. The units are in percentage 
 stator3D.lean(leanX=[0,0.01,-0.02],leanZ=[0,0.5,1])
-stator3D.create_blade(nProfiles=20,profile_points=160,20)
+stator3D.create_blade(nProfiles=20,profile_points=160,trailing_edge_points=20)
 # stator3D.plot3D()
 print('check')
 stator3D.export_solidworks('rotor')