(tests) Updated transonic rae mesh and test results

blast/validation/raeValidation.py

@@ -43,7 +43,7 @@ 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' : 0.008, 'msLe' : 0.002}, # parameters for input file model
     'Dim' : 2, # problem dimension
     'Format' : 'gmsh', # save format (vtk or gmsh)
     # Markers
@@ -139,12 +139,11 @@ def main():
     # Test solution
     print(ccolors.ANSI_BLUE + 'PyTesting...' + ccolors.ANSI_RESET)
     tests = CTests()
-    tests.add(CTest('Cl', isol.getCl(), 0.740, 5e-2))
-    tests.add(CTest('Cd wake', vsol.Cdt, 0.0096, 1e-3, forceabs=True))
-    tests.add(CTest('Cd integral', isol.getCd() + vsol.Cdf, 0.0132, 1e-3, forceabs=True))
+    tests.add(CTest('Cl', isol.getCl(), 0.730, 5e-2))
+    tests.add(CTest('Cd wake', vsol.Cdt, 0.0098, 1e-3, forceabs=True))
+    tests.add(CTest('Cd integral', isol.getCd() + vsol.Cdf, 0.0126, 1e-3, forceabs=True))
     tests.add(CTest('Cdf', vsol.Cdf, 0.0067, 1e-3, forceabs=True))
-    if icfg['LSolver'] == 'SparseLu':
-        tests.add(CTest('Iterations', len(aeroCoeffs['Cl']), 34, 0, forceabs=True))
+    tests.add(CTest('Iterations', len(aeroCoeffs['Cl']), 34, 0, forceabs=True))
     tests.run()
 
     expResults = np.loadtxt(os.path.dirname(os.path.dirname(os.path.abspath(__file__))) + '/models/references/rae2822_AR138_case6.dat')