|
=0 2D, =1 AXISYMMETRIC
|
|
|
=0 Euler, =1 Navier-Stokes
|
|
|
Reynolds by meter (the mesh is given in meter)
|
|
|
inverse of Froude number (=0 no gravity)
|
|
|
inflow Mach number
|
|
|
ratio pout/pin
|
|
|
wall =1 newmann b.c. on the temp.(adiabatic wall), =2 Dirichlet.(isothermal wall)
|
|
|
inflow temperature (in Kelvin) for Sutherland laws
|
|
|
if isothermal walls , wall temperature (in Kelvin)
|
|
|
angle of attack
|
|
|
Euler fluxes =1 roe, =2 osher,=3 kinetic
|
|
|
nordre = 1 first order scheme, =2 second order, =3 limited second order
|
|
|
=0 global time steping (unsteady), =1 local Euler, =2 local N.S.
|
|
|
cfl
|
|
|
number of time steps
|
|
|
frequence for the solution to be saved
|
|
|
maximum physical time for run (for unsteady problems)
|
|
|
order of magnitude for the residual to be reduced (for steady problems)
|
|
|
=0 start with uniform solution, =1 restart from INIT_NS
|
|
|
=0 no turbulence model, =1 k-epsilon model
|
|
|
=0 two-layer technique, =1 wall laws
|
|
|
delta in wall laws or limit of the one-eq. model. (in meter)
|
|
|
=0 start from uniform solution for k-epsilon, =1 from INIT_KE
|
|
|
xtmin,xtmax,ytmin,ytmax (BOX for k-epsilon r.h.s)
|
|
