Ejector Nozzle, Viscous
Spalart-Allmaras Turbulence Model

Freestream total  0.20 14.73 550.0 0. 0.

Turbulence Spalart

CFL AUTO DECREASE 2 CFLMAX 100
DQ LIMITER ON RELAX 0.1
FIXER ZONE ALL

CYCLES 8000
ITER_CYCLE 1
CONVERGE ORDER 10

IMPLICIT BOUNDARY ON
IMPLICIT UGAUSS LINE EXACT_LHS VISCOUS_JACOBIAN FULL CONVERGE FREQUENCY 11 SUBITERATIONS 6

RHS HLLE SECOND

GRADIENT LEAST_SQUARES

TVD VENKAT 3.0 KVENKAT 0

/Jet Inflow
ARBITRARY INFLOW
total 
ZONE 1 
USURFACE 4 0.07 35.73 644.0 0. 0.
END INFLOW

DOWNSTREAM PRESSURE 13.45 ZONE 1

WALL SLIP 1

LOADS
  print totals zones plane lift drag
  reference area 1.0
  reference length 1.0
  reference moment center 0.0 0.0 0.0
  include ejector.loads
ENDLOADS

IMPLICIT BOUNDARY ON

/DEBUG  3  1  / Print 'actual' RHS residual
/DEBUG 41  1  / Enable Implicit coupling, for running dedicated
/DEBUG 42  1  / Cycle-time efficiency, gradient calculated once between the N-S and turbulence mode pass, not coupled
/DEBUG 46  6  / Face gradient correction, more stable viscous flux discretization than 46 1

/TEST 51 50   / Set mu_t limit to 50,000


END