Seiner Convergent-Divergent Nozzle
 Turbulent flow - 104 deg. F Test
 Unstructured Grid from Boeing (Andy Dorgan), Axisymmetric Flow

/----Numerics--------------------
 convergence level 1.0e-9
/ cycles 1001
 cycles 101
 iterations per cycle 5
 cfl auto decrease 2 cflmax 1000
/ cfl auto decrease 2 cflmax 200
/ cfl auto decrease 2 cflmax 100
/ cfl auto cflmin 1 cflmax 100
 dq limiter on relax 0.50
/ rhs hll first
 rhs hlle second
 gradient least_squares
 rhs viscous full
 tvd barth 3.0
/ q limit pressuremin 0.05 pressuremax 100 densitymin 0.05 densitymax 100
 q limit pressuremin 0.05 pressuremax 20 densitymin 0.05 densitymax 20
 fixer average zone all
 implicit boundary on
 implicit ugauss line exact_lhs viscous_jacobian full converge frequency 11 subiterations 6

/----Freestream Conditions--------------------
 prandtl 0.72 0.70
 freestream static 0.01 14.7 530.0 0.0 0.0

/----Arbitrary Inflow--------------------
 arbitrary inflow
  total
  hold_totals 
  zone 1
    usurface 4 0.2 115.02 563.66 0.0 0.0
 endinflow

/----Outflow Conditions--------------------
 downstream pressure freestream extrapolate supersonic zone all

/----Viscous Terms--------------------
 turbulence sst

/----Test Options--------------------


 end