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1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 | 0 --> =0 2D, =1 AXISYMMETRIC
0 --> =0 Euler, =1 Navier-Stokes
1.e2 --> Reynolds by meter (the mesh is given in meter)
0. --> inverse of Froude number (=0 no gravity)
0.8 --> inflow Mach number
1. --> ratio pout/pin
1 --> wall =1 newmann b.c.(adiabatic wall), =2 (isothermal wall)
300. --> inflow temperature (in Kelvin) for Sutherland laws
288. --> if isothermal walls , wall temperature (in Kelvin)
0.0 --> angle of attack
1 --> Euler fluxes =1 roe, =2 osher,=3 kinetic
3 --> nordre = 1st order scheme, =2 2ndorder, =3 limited 2nd order
1 --> =0 global time steping (unsteady), =1 local Euler, =2 local N.S.
1. --> cfl
LastIteration --> number of time step
500 --> frequence for the solution to be saved
1.e10 --> maximum physical time for run (for unsteady problems)
-4. --> order of magnitude for the residual to be reduced (for steady problems)
INIT --> =0 start with uniform solution, =1 restart from INIT_NS
cccc turbulence ccccccccccccccccccccccccccccccccccccccccccccccccccccccc
0 --> =0 no turbulence model, =1 k-epsilon model
0 --> =0 two-layer technique, =1 wall laws
1.e-2 --> delta in wall laws or limit of the one-eq. model. (in meter)
0 --> =0 start from uniform solution for k-epsilon, =1 from INIT_KE
-1.e10 1.e10 -1.e10 1.e10 --> xtmin,xtmax,ytmin,ytmax (BOX for k-epsilon r.h.s)
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