Released 1.0.17

Fixes to stage tutorial.

pyproject.toml

@@ -1,14 +1,14 @@
 [tool.poetry]
 name = "pyturbo-aero"
-version = "1.0.16"
+version = "1.0.17"
 description = "PyTurbo_Aero is a Turbomachinery blade design library that lets you create a full 3D blades and passages."
 authors = ["Paht Juangphanich <paht.juangphanich@nasa.gov>"]
 packages = [
     { include = "pyturbo" }
 ]
 
 [tool.poetry.dependencies]
-python = ">=3.9"
+python = ">=3.10"
 plotly = "*"
 tqdm = "*"
 scipy = "*"

pyturbo/aero/__init__.py

@@ -1,7 +1,7 @@
 """ 
     Imports airfoil 2D and 3D and wavy  
 """
-from .airfoil2D import *
-from .airfoil3D import *
-from .airfoil_wavy import *
-from .passage2D import *
+from .airfoil2D import Airfoil2D
+from .airfoil3D import Airfoil3D, stack_type,spline_type
+from .airfoil_wavy import Airfoil3D_Wavy
+from .passage2D import Passage2D

pyturbo/aero/airfoil_wavy.py

@@ -5,7 +5,7 @@
 from ..helper import derivative_1, bezier,cosd,sind
 import math
 
-class airfoil_wavy(Airfoil3D):
+class Airfoil3D_Wavy(Airfoil3D):
     """Makes the surface of the airfoil: LE, TE, SS, PS wavy
     """
     def __init__(self,profileArray,profile_loc,height):
@@ -16,7 +16,7 @@ def __init__(self,profileArray,profile_loc,height):
             profile_loc ([List[float]]): Locations in terms of percent span where these 2D airfoils are located 
             height ([float]): height of the airfoil
         """
-        super(airfoil_wavy, self).__init__(profileArray,profile_loc,height)
+        super(Airfoil3D_Wavy, self).__init__(profileArray,profile_loc,height)
 
 
     def stretch_thickness_chord(self,SSRatio,PSRatio,LERatio,TERatio,LE_wave_angle,TE_wave_angle,TE_smooth=0.85):

pyturbo/aero/passage2D.py

@@ -11,10 +11,10 @@
 import matplotlib.pyplot as plt
 from mpl_toolkits.mplot3d import Axes3D
 
-class passage2D:
+class Passage2D:
     """Passage2D fits 3D blades inside of a channel
     """
-    def __init__(self,airfoil_array,spacing_array,periodicity_array):
+    def __init__(self,airfoil_array,spacing_array):
         '''
         Initialize the passage with airfoils and spacing array
             airfoil_array = array of airfoil3D objects
@@ -24,7 +24,6 @@ def __init__(self,airfoil_array,spacing_array,periodicity_array):
         '''
         self.airfoils=airfoil_array
         self.spacing=spacing_array
-        self.periodicity_array = periodicity_array
 
 
     def add_endwalls(self,zhub:List[float],rhub:List[float],zshroud:List[float],rshroud:List[float],zhub_control:List[float]=[],rhub_control:List[float]=[],zshroud_control:List[float]=[],rshroud_control:List[float]=[]):

pyturbo/helper/bezier.py

@@ -146,7 +146,7 @@ def get_point_dt(self,t):
                 tempy = self.y[1]- self.y[0]          
             else:
                 for j in range(self.n-1): # n-1      
-                    b = (comb(self.n-2,j,True)*t[i]**j) * (1-t[i])**(self.n-2-j)    # Bn-1                    
+                    b = (comb(self.n-2,j,exact=True)*t[i]**j) * (1-t[i])**(self.n-2-j)    # Bn-1                    
                     tempx = tempx + b*(self.x[j+1]-self.x[j]) # Note: j+1 = j
                     tempy = tempy + b*(self.y[j+1]-self.y[j])