Turbulent Flat Plate Boundary Layer
M = 0.2, S-A

/ Inlet Mach number, pressure (psi), temperature (deg R), alpha, beta
Freestream static 0.2   14.7   530.   0.   0.

/ Viscous terms
Turbulence Spalart
/Turbulence SST

CFL AUTO DECREASE 2 CFLMAX 500
DQ LIMITER ON RELAX 0.1
 FIXER average

/ Numerics
CYCLES 3000
ITER_CYCLE 1
CONVERGE ORDER 10

IMPLICIT BOUNDARY ON
IMPLICIT UGAUSS LINE EXACT_LHS VISCOUS_JACOBIAN FULL SUBITERATIONS 6
/what is this?

RHS HLLE SECOND

GRADIENT LEAST_SQUARES

TVD BARTH 3.0
/read the paper?

/ Boundary conditions
DOWNSTREAM PRESSURE FREESTREAM ZONE 1

WRITE VARIABLES CF

END