Boman Romain
--- a/flow/cases/wbht.py

+ 3

− 3
+++ b/flow/cases/wbht.py

+ 3

− 3
 @@ -5,7 +5,7 @@
 # @authors Adrien Crovato
 #
 # CAUTION
-# Results might be nonphysical!
+# Gmsh might not generate the wing/tail surfaces properly. Results might not be accurate 

 def getParam():
    p = {}
 @@ -34,7 +34,7 @@ def getParam():
                 'msFus' : fums, 'msFusCaps' : fucms, 'msFar' : fams} # Parameters for input file model
    p['Dim'] = 3 # Problem dimension
    p['Format'] = 'vtk' # Save format (vtk or gmsh)
-    p['Slice'] = [0.83, 3.0, 4., 6.1, 6.9] # array of (y) coordinates to perform slice along the span (empty if none)
+    p['Slice'] = [0.83, 3.0, 4.0, 6.2, 6.9] # array of (y) coordinates to perform slice along the span (empty if none)
    p['TagId'] = 9 # tag number of physical group to be sliced
    # Markers
    p['Fluid'] = 'field' # Name of physical group containing the fluid
 @@ -46,7 +46,7 @@ def getParam():
    p['WakeTips'] = ['wakeTipW', 'wakeTipT'] # LIST of names of physical group containing the edge of the wake
    p['TeTips'] = ['teTipW', 'teTipT'] # LIST of names of physical group containing the edge of the wake and the trailing edge
    # Freestream
-    p['M_inf'] = 0.6 # Freestream Mach number
+    p['M_inf'] = 0.75 # Freestream Mach number
    p['CL'] = 0.4 # Target lift coefficient
    p['AoA'] = 0. # Freestream angle of attack (guess)
    p['dCL'] = 7.5 # Slope of CL w.r.t AoA [1/rad] (guess)