Shock Wave Boundary Layer Interaction
Unstructured Validation
Freestream Mach 5, 10 degree deflection angle

/ '/' is used to comment in the this file. The options marked
/ 'default/s' were used in the previous unstructured validation studies,
/ however some of those option are now default. These options have been
/ commented out but left in this file to inform users of this new
/ behavior.


GAS 1.400 .72 .9 1716. 

/ SPAWN ------------------------------------------------
SPAWN "./post_process2" FREQUENCY 2000

/ BOUNDARY CONDITIONS ----------------------------------
Freestream TOTAL conditions 5.  307.48  738.00  0.0 0.0
Downstream pressure extrapolate zone all

Wall Temperature 540.00 zone all


/ VISCOUS TERMS ----------------------------------------
turbulence spalart
/turbulence sst 

mut limiter 50

/ NUMERICS ---------------------------------------------
cycle 29000
/iterations per cycle 1 default
converge order 10
cfl auto decrease 2 cflmin 1 cflmax 500
fixer zone all

/rhs hlle second /default
/rhs viscous thin-layer /default
/implicit boundary on /default
implicit ugauss line exact_lhs viscous_jacobian full   /defaults, converge frequency 11 subiterations 6
/gradient least_squares /default

/tvd barth 3.0 default

SOLVER-STAGES
 RESTART_STAGES
 STEP FIRST
  SOLVER NAVIER-STOKES
   SET RHS TO HLLE FIRST
   SET CYCLES TO 1000
  END SOLVER
 END STEP
 STEP SECOND
 END STEP
END SOLVER-STAGES


write variables cf

loads
  print totals lift drag frequency 10
  zone 1  
  surface u 4 force viscous
endloads


END