Files with data from FUN3D solutions along lines on Family II finest four grids:

n0012II.x_y.dat
   x = grid level (1=finest, 2=2nd finest, 3=3rd finest, 4=4th finest)
   y = location (x10=x/c of 10, x1.001=x/c of 1.001, x0.999L=x/c of 0.999 lower surface,
                 x0.999U=x/c of 0.999 upper surface, z.00008=z/c=0.00008, z0=z/c of zero behind the airfoil)

   e.g.:  n0012II.2_x10.dat gives data on the 2nd finest grid along line x/c=10

Variables of interest are:
"cp" - pressure coefficient
"u" - u-component of velocity (nondimensionalized by freestream speed of sound)
"w" - w-component of velocity (nondimensionalized by freestream speed of sound)
"mu_t" - eddy viscosity (nondimensionalized by freestream laminar mu)
"turb1" - Spalart-Allmaras model's SA-neg turbulence variable nu_t (nondimensionalized by freestream laminar nu)
 
Note that the data are in Tecplot format, and may not be sorted (Tecplot can sort the data when plotting).
