(tests) Updated 2D transonic RAE mesh

Increased number of elements in the TE region and updated tests values.

blast/validation/raeValidation.py

@@ -42,7 +42,7 @@ def cfgInviscid(nthrds, verb):
     'Verb' : verb, # verbosity
     # Model (geometry or mesh)
     'File' : os.path.dirname(os.path.dirname(os.path.abspath(__file__))) + '/models/dart/rae_2.geo', # Input file containing the model
-    'Pars' : {'xLgt' : 50, 'yLgt' : 50, 'msF': 10, 'msTe' : 0.01, 'msLe' : 0.001}, # parameters for input file model
+    'Pars' : {'xLgt' : 50, 'yLgt' : 50, 'msF': 10, 'msTe' : 0.0075, 'msLe' : 0.001}, # parameters for input file model
     'Dim' : 2, # problem dimension
     'Format' : 'gmsh', # save format (vtk or gmsh)
     # Markers
@@ -64,7 +64,7 @@ def cfgInviscid(nthrds, verb):
     'y_ref' : 0.0, # reference point for moment computation (y)
     'z_ref' : 0.0, # reference point for moment computation (z)
     # Numerical
-    'LSolver' : 'PARDISO', # inner solver (Pardiso, MUMPS or GMRES)
+    'LSolver' : 'SparseLu', # inner solver (Pardiso, MUMPS or GMRES)
     'G_fill' : 2, # fill-in factor for GMRES preconditioner
     'G_tol' : 1e-5, # tolerance for GMRES
     'G_restart' : 50, # restart for GMRES
@@ -132,14 +132,12 @@ def main():
     # Test solution
     print(ccolors.ANSI_BLUE + 'PyTesting...' + ccolors.ANSI_RESET)
     tests = CTests()
-    tests.add(CTest('Cl', isol.getCl(), 0.766, 5e-2))
+    tests.add(CTest('Cl', isol.getCl(), 0.759, 5e-2))
     tests.add(CTest('Cd wake', vsol.Cdt, 0.0093, 1e-3, forceabs=True))
-    tests.add(CTest('Cd integral', isol.getCd() + vsol.Cdf, 0.0138, 1e-3, forceabs=True))
-    tests.add(CTest('Cdf', vsol.Cdf, 0.0069, 1e-3, forceabs=True))
-    # if icfg['LSolver'] == 'PARDISO':
-    #     tests.add(CTest('Iterations', len(aeroCoeffs['Cl']), 43, 0, forceabs=True))
-    # elif icfg['LSolver'] == 'SparseLu':
-    #     tests.add(CTest('Iterations', len(aeroCoeffs['Cl']), 42, 0, forceabs=True))
+    tests.add(CTest('Cd integral', isol.getCd() + vsol.Cdf, 0.0134, 1e-3, forceabs=True))
+    tests.add(CTest('Cdf', vsol.Cdf, 0.0068, 1e-3, forceabs=True))
+    if icfg['LSolver'] == 'SparseLu':
+        tests.add(CTest('Iterations', len(aeroCoeffs['Cl']), 29, 0, forceabs=True))
     tests.run()
 
     expResults = np.loadtxt(os.path.dirname(os.path.dirname(os.path.abspath(__file__))) + '/models/references/rae2822_AR138_case6.dat')