opencfd-scu.in

# OpenCFD-SCU-Ver1.00 input file 
GRID_3D = 25   240   20
PARALLEL_3D = 1   1   1
STREAM = 0
CHARTERIC = 0
TEST = 0

IPERIODIC = 0   0   1
JAC_BOUND = 1   1   1
DIF_BOUND = 0   1   0   1   0   0
NON_REFLETION = 0   1   0   1   0   0

SCHEME_INVIS = WENO7_SYMBO
#SCHEME_INVIS = NND2
SCHEME_VIS = CD8
#SCHEME_INVIS = SCHEME_HYBRIDAUTO
HY_DP_INTV = 0.01 0.2
HY_SMOOTH_DP = 0
HY_STYLE = 2
HY_PATCH_ZONE = 0
HY_ZONE0 = 10   25   100   240   5   20   20.0


RE = 5581.4
AMA = 2.9
GAMMA = 1.40
PR = 0.70
T_REF = 108.1
EPSL_SW = 0.0

DT = 0.01
END_TIME = 10
KSTEP_SHOW = 1
KSTEP_SAVE = 1000
INIT_STAT = 1

IBC = 108
#mzmax, mtmax, Inlet_boundary, If_wall_not_normal
BC_NPARA = 10   5   1   0

#Tw, epsl, x_dis_begin, x_dis_end, beta, x_wall_begin, x_up_bound_begin, SLZ
BC_RPARA = 2.84   0.2   -320.   -300   0.1   -400.   -50.   14.  


#nstep_filter, Filter_X, Filter_Y, Filter_Z, ib, ie, jb, je, kb, ke, Filter_scheme  // s0, rth, Filter_end_time
#FILTER_NPARA0 = 100   1   1   1   0   25   0   240   0   20   2
#FILTER_RPARA0 = 1.0   1.e-5   1000000


#ANA_EVENT0 = 101   1
#ANA_EVENT1 = 105   10
#ANA_NPARA1 = 2   5   10   15
#ANA_EVENT2 = 107   10
#ANA_NPARA0 = 0
#ANA_RPARA0 = 0

















#*****************************************************************************************************
# IBC  nk   nr  IF_symmetry  IF_withleading   Iflag_upperboundary    AoA  Tw     epsl_wall epsl_upper  wall_dis_begin wall_dis_end  //(liftbody)
  124   3    6        1              0                 1               0.  3.797     0.02        0.          50.           60.