[Amber0922]

I try to run the backward step model, but comes to some questions. When I try to run my config file, it shows

Error in "void CSolver::SetResidual_RMS(const CGeometry*, const CConfig*)":
-------------------------------------------------------------------------
SU2 has diverged (NaN detected).
-------------------------------------------------------------------------

I think maybe I forget to set something, but I don't find it. Here is my config file.



% Physical governing equations (EULER, NAVIER_STOKES,
% WAVE_EQUATION, HEAT_EQUATION, FEM_ELASTICITY,
% POISSON_EQUATION)
SOLVER= RANS
KIND_TURB_MODEL= SA
HYBRID_RANSLES= SA_EDDES
%
% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT)
MATH_PROBLEM= DIRECT
%
% Axisymmetric simulation, only compressible flows (NO, YES)
AXISYMMETRIC= NO
%
% Restart solution (NO, YES)
RESTART_SOL= NO

SYSTEM_MEASUREMENTS= SI
%
% ----------- COMPRESSIBLE AND INCOMPRESSIBLE FREE-STREAM DEFINITION ----------%
%
MACH_NUMBER= 0.128
AOA= 0.0
SIDESLIP_ANGLE= 0.0
FREESTREAM_TEMPERATURE= 298.3
FREESTREAM_VELOCITY= ( 44.2, 0.00, 0.00 )
REYNOLDS_NUMBER= 36000
REYNOLDS_LENGTH= 1.0
%
% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
%
% Reference origin for moment computation
REF_ORIGIN_MOMENT_X = 0.25
REF_ORIGIN_MOMENT_Y = 0.00
REF_ORIGIN_MOMENT_Z = 0.00
%
% Reference length for pitching, rolling, and yawing non-dimensional moment
REF_LENGTH= 1.0
%
% Reference area for force coefficients (0 implies automatic calculation)
REF_AREA= 0
%
% ------------------------- UNSTEADY SIMULATION -------------------------------%

TIME_DOMAIN= YES
TIME_MARCHING= DUAL_TIME_STEPPING-2ND_ORDER
%
% U_inf = 69.4448 - dt*=0.02 - dt=0.000288
TIME_STEP= 0.00046
MAX_TIME= 0.689
UNST_CFL_NUMBER= 0.0
INNER_ITER= 80
%
% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%

MARKER_HEATFLUX= ( STEP, 0.0, UPPERWALL,0.0, LOWERWALL,0.0 )
flow_direction_x,

MARKER_INLET= ( INLET, 298.3, 44.2, 1.0, 0.0, 0.0 )

MARKER_SYM= ( WALL1, WALL2 )

MARKER_OUTLET= ( OUTLET, 0.0 )

MARKER_PLOTTING= ( STEP, WALL1, WALL2, UPPERWALL, LOWERWALL)

MARKER_MONITORING= ( STEP, WALL1, WALL2, UPPERWALL, LOWERWALL )

% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%

NUM_METHOD_GRAD= GREEN_GAUSS

CFL_NUMBER= 10.0

CFL_ADAPT= NO

CFL_ADAPT_PARAM= ( 1.5, 0.5, 2.0, 100.0 )

RK_ALPHA_COEFF= ( 0.66667, 0.66667, 1.000000 )
TIME_ITER= 2000
%

% ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
%
MUSCL_FLOW= YES
SLOPE_LIMITER_FLOW= NONE
MUSCL_TURB= NO
VENKAT_LIMITER_COEFF= 0.05

% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
%
CONV_NUM_METHOD_FLOW= SLAU2
TIME_DISCRE_FLOW= EULER_IMPLICIT
%
% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
%
CONV_NUM_METHOD_TURB= SCALAR_UPWIND
TIME_DISCRE_TURB= EULER_IMPLICIT

% --------------------------- CONVERGENCE PARAMETERS --------------------------%
%
CONV_RESIDUAL_MINVAL= -15
CONV_STARTITER= 10
CONV_CAUCHY_ELEMS= 100
CONV_CAUCHY_EPS= 1E-6

MESH_FILENAME= backwardstep.cgns

MESH_FORMAT= CGNS

MESH_OUT_FILENAME= mesh_out.su2

SOLUTION_FILENAME= solution_flow.dat

SOLUTION_ADJ_FILENAME= solution_adj.dat

TABULAR_FORMAT= TECPLOT

CONV_FILENAME= history

RESTART_FILENAME= restart_flow.dat

RESTART_ADJ_FILENAME= restart_adj.dat

VOLUME_FILENAME= flow

VOLUME_ADJ_FILENAME= adjoint

SURFACE_FILENAME= surface_flow
SURFACE_ADJ_FILENAME= surface_adjoint

SCREEN_OUTPUT=(TIME_ITER, INNER_ITER, LIFT, DRAG, TOTAL_HEATFLUX)