version4.0
Lines 1: 3 lines of characters identifying the aerodynamic data




Line 2: Reference aerodynamic parameters (depends on value of i_flow in .con file)
ref_n      ref_mass    ref_d     ref_pr or ref_pd
{0}        {1}         {2}         {3}

Line 3: Reynolds number or dynamic viscosity
ref_mue
{4}

Line 4:  Fluid data (depends on value of i_fluid in .con file)
cp_gas       gamma_gas     (i-fluid = 1, ideal gas)
{5}          {6}

Line 5 :  Number of points on inlet boundary where flow conditions are specified
n_inbc
1

Line 6:  Fraction of inlet boundary where flow conditions are specified (n_inbc values)
f_inbc
0.0

Line 7:  Pressure on inlet boundary (n_inbc values which depend on i_bc in .con file)
pt_inbc   (i_bc = 0)
{7}

Line 8:  Temperature on inlet boundary (n_inbc values, depend on i_bc in .con file)
tt_inbc   (i_bc = 0) 
{8}

Line 9:  Swirl on inlet boundary (n_inbc values, depend on i_bc in .con file)
rcu_inbc  (i_bc = 0)
{9}

Line 10: Mixing model and blade transparency model parameters
eddy      f_bl_le      f_bl_te
{10}      0.0          0.0
