Sample Case: 10 Deg Diamond Airfoil in Supersonic Flow                
 &FLOW_VARS
 XMINF   =   2.000000    ,
 PITCH   =   5.000000    , 
 /
 &GRID_VARS
 IGRID   =           4,
 NBMIN   =          64,
 NADAPT  =         100,
 NASTART =         100,
 NASTOP  =         800,
 ACLIMIT =   3.000000    ,
 AMIND   =  0.3000000    ,
 AMAXD   =   1.000000    ,
 /
 &SCHEME_VARS
 IRESTART        =           0,
 NMAX    =        5000,
 ITSCHEME        =           1,
 IDTCONST        =           1,
 NCSTART =         200,
 NCEND   =         400,
 CFLSTART        =   1.000000    ,
 CFLEND  =   4.000000    ,
 NWRITE  =         200,
 NLWRITE =          10,
 IFSCHEME        =           3,
 EPS     =   1.000000    ,
 XK      =  -1.000000    ,
 ILIM    =           1,
 IWALLBC =           0,   ,
 AREAREF =   1.000000    ,
 /