(format) Renamed OpenMDAO api

blast/api/mdaAPI.py → blast/api/mda_api.py

@@ -23,7 +23,7 @@ import numpy as np
 from fwk.coloring import ccolors
 import openmdao.api as om
 import blast
-import blast.utils as viscUtils
+import blast.utils as vutils
 from pygeo import DVGeometryCST
 from scipy.optimize import least_squares
 import fwk
@@ -185,7 +185,7 @@ class BlasterSolver(om.ExplicitComponent):
 
     def __write(self, sfx='0'):
         sfx = '_'+sfx
-        viscUtils.getSolution(self.isol.sec, write=True, toW=['x', 'y', 'cf'], sfx=sfx) # Boundary layer
+        vutils.getSolution(self.isol.sec, write=True, toW=['x', 'y', 'cf'], sfx=sfx) # Boundary layer
         self.isol.writeCp(sfx=sfx) # Cp
         self.isol.iobj['wrt'].save(self.isol.iobj['pbl'].msh.name + sfx) # Mesh
         self.isol.save(sfx) # Solution
@@ -473,12 +473,6 @@ class BlasterFFDGeometry(om.ExplicitComponent):
         # Fit circle to leading edge points
         center, radius = self.fit_circle(le_points_combined[:, 0], le_points_combined[:, 1])
 
-        # print('Upper shape', inputs['upper_shape'])
-        # print('Lower shape', inputs['lower_shape'])
-        # print('Max thickness', round(maxThickness, 4))
-        # print('Center:', center)
-        # print('Radius:', radius)
-
         # Go back to normal mesh
         x_aero_out = np.zeros(len(inputs['x_aero0']))
         for i, val in enumerate(self.options['nodeRows']):

blast/mdao/opti_NACA.py

-import blast.utils as viscUtils
+import blast.utils as vutils
 import numpy as np
 
 from fwk.wutils import parseargs
@@ -6,8 +6,8 @@ import fwk
 from fwk.testing import *
 from fwk.coloring import ccolors
 
-from blast.api.mdaAPI import BlasterSolver
-from blast.api.mdaAPI import BlasterModeUpdater
+from blast.api.mda_api import BlasterSolver
+from blast.api.mda_api import BlasterModeUpdater
 
 import openmdao.api as om
 

blast/mdao/opti_subsonic.py

-import blast.utils as viscUtils
+import blast.utils as vutils
 import numpy as np
 
 from fwk.wutils import parseargs
@@ -6,8 +6,8 @@ import fwk
 from fwk.testing import *
 from fwk.coloring import ccolors
 
-from blast.api.mdaAPI import BlasterSolver
-from blast.api.mdaAPI import BlasterModeUpdater
+from blast.api.mda_api import BlasterSolver
+from blast.api.mda_api import BlasterModeUpdater
 
 import openmdao.api as om
 
@@ -34,7 +34,6 @@ def cfgInviscid(nthrds, verb):
     'Wake' : 'wake', # LIST of names of physical group containing the wake
     'WakeTip' : 'wakeTip', # LIST of names of physical group containing the edge of the wake
     'Te' : 'te', # LIST of names of physical group containing the trailing edge
-    'dbc' : False,
     'Upstream' : 'upstream',
     # Freestream
     'M_inf' : 0.1, # freestream Mach number

blast/mdao/opti_transonic.py

-import blast.utils as viscUtils
+import blast.utils as vutils
 import numpy as np
 
 from fwk.wutils import parseargs
@@ -6,8 +6,8 @@ import fwk
 from fwk.testing import *
 from fwk.coloring import ccolors
 
-from blast.api.mdaAPI import BlasterSolver
-from blast.api.mdaAPI import BlasterModeUpdater
+from blast.api.mda_api import BlasterSolver
+from blast.api.mda_api import BlasterModeUpdater
 
 import openmdao.api as om
 
@@ -34,7 +34,6 @@ def cfgInviscid(nthrds, verb):
     'Wake' : 'wake', # LIST of names of physical group containing the wake
     'WakeTip' : 'wakeTip', # LIST of names of physical group containing the edge of the wake
     'Te' : 'te', # LIST of names of physical group containing the trailing edge
-    'dbc' : False,
     'Upstream' : 'upstream',
     # Freestream
     'M_inf' : 0.78, # freestream Mach number