diff --git a/blast/api/mdaAPI.py b/blast/api/mda_api.py similarity index 98% rename from blast/api/mdaAPI.py rename to blast/api/mda_api.py index 9535530694732a14624406cc89f60643dcb40b5f..6918badec5cb70d3bda498e102b197543c28bbf7 100644 --- a/blast/api/mdaAPI.py +++ b/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']): diff --git a/blast/mdao/opti_NACA.py b/blast/mdao/opti_NACA.py index e14e0f217894f4925efa241645eed99b1c831f9e..7a8729ad4dd1306a6ce41c1a3822de91815a2073 100644 --- a/blast/mdao/opti_NACA.py +++ b/blast/mdao/opti_NACA.py @@ -1,4 +1,4 @@ -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 diff --git a/blast/mdao/opti_subsonic.py b/blast/mdao/opti_subsonic.py index 2228498dc3bf89be4d9c8b264c1c3e6a287723b9..a5f86f6555367f00bf90224dbe9ce9d7041c37d2 100644 --- a/blast/mdao/opti_subsonic.py +++ b/blast/mdao/opti_subsonic.py @@ -1,4 +1,4 @@ -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 diff --git a/blast/mdao/opti_transonic.py b/blast/mdao/opti_transonic.py index 5a91629481068fc25843357759c77f1bcb0a99ec..b88660987758f6261fb7013ea1315959f9c4c7a7 100644 --- a/blast/mdao/opti_transonic.py +++ b/blast/mdao/opti_transonic.py @@ -1,4 +1,4 @@ -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