Fix biparabolic regression

TestCases/euler/biparabolic/BIPARABOLIC.cfg

@@ -33,24 +33,24 @@ REF_AREA= 1.0
 % ------------------------ SUPERSONIC SIMULATION ------------------------------%
 %
 EQUIV_AREA= YES
-EA_INT_LIMIT= ( -100.0, 100.0, 2.0 )
+EA_INT_LIMIT= ( 1.562, 4.562, 2.0 )
 
 % ----------------------- BOUNDARY CONDITION DEFINITION -----------------------%
 %
 MARKER_EULER= ( airfoil )
 MARKER_FAR= ( farfield )
-MARKER_NEARFIELD= ( upper_nearfield, lower_nearfield )
+MARKER_NEARFIELD= ( nearfield )
 MARKER_PLOTTING= ( airfoil )
-MARKER_MONITORING= ( airfoil, upper_nearfield )
+MARKER_MONITORING= ( airfoil )
 
 % ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
 %
 NUM_METHOD_GRAD= GREEN_GAUSS
 CFL_NUMBER= 25.0
 CFL_ADAPT= NO
-CFL_ADAPT_PARAM= ( 1.5, 0.5, 1.0, 100.0 )
+CFL_ADAPT_PARAM= ( 0.5, 1.5, 1.0, 100.0 )
 RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
-EXT_ITER= 99999999
+ITER= 1000
 
 % -------------------------- MULTIGRID PARAMETERS -----------------------------%
 %

TestCases/serial_regression.py

@@ -122,6 +122,14 @@ def main():
     wedge.test_vals = [-4.350066, 1.379784, -0.249526, 0.043953]
     test_list.append(wedge)
 
+    # Supersonic biparabolic airfoil
+    biparabolic           = TestCase('biparabolic')
+    biparabolic.cfg_dir   = "euler/biparabolic"
+    biparabolic.cfg_file  = "BIPARABOLIC.cfg"
+    biparabolic.test_iter = 25
+    biparabolic.test_vals = [-2.177255, 0.461450, 0.278865, 3.447917]
+    test_list.append(biparabolic)
+
     # ONERA M6 Wing
     oneram6           = TestCase('oneram6')
     oneram6.cfg_dir   = "euler/oneram6"