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Added HL CRM config and new post.
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‎_posts/2018-02-14-v6.md

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---
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layout: post
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title: "Official Release of SU2 v6.0"
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author: SU2 Team
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---
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View the [official announcement](../../../../../emails/su2_email_v6.html).

‎documents/turb_hl_crm.cfg

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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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% %
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% SU2 configuration file %
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% Case description: Turbulent flow past the High-Lift CRM (AoA = 8 deg) %
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% Author: Thomas D. Economon %
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% Date: 2018.02.14 %
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% File Version 6.0.0 "Falcon" %
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% %
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%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%
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% ------------- DIRECT, ADJOINT, AND LINEARIZED PROBLEM DEFINITION ------------%
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%
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% Physical governing equations (EULER, NAVIER_STOKES,
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% WAVE_EQUATION, HEAT_EQUATION, LINEAR_ELASTICITY,
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% POISSON_EQUATION)
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PHYSICAL_PROBLEM= NAVIER_STOKES
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%
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% Specify turbulence model (NONE, SA, SA_NEG, SST)
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KIND_TURB_MODEL= SA
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%
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% Mathematical problem (DIRECT, CONTINUOUS_ADJOINT, DISCRETE_ADJOINT)
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MATH_PROBLEM= DIRECT
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%
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% Restart solution (NO, YES)
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RESTART_SOL= NO
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%
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% Regime type (COMPRESSIBLE, INCOMPRESSIBLE)
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REGIME_TYPE= COMPRESSIBLE
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%
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% System of measurements (SI, US)
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% International system of units (SI): ( meters, kilograms, Kelvins,
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% Newtons = kg m/s^2, Pascals = N/m^2,
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% Density = kg/m^3, Speed = m/s,
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% Equiv. Area = m^2 )
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% United States customary units (US): ( inches, slug, Rankines, lbf = slug ft/s^2,
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% psf = lbf/ft^2, Density = slug/ft^3,
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% Speed = ft/s, Equiv. Area = ft^2 )
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SYSTEM_MEASUREMENTS= US
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% -------------------- COMPRESSIBLE FREE-STREAM DEFINITION --------------------%
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%
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% Mach number (non-dimensional, based on the free-stream values)
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MACH_NUMBER= 0.2
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%
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% Angle of attack (degrees, only for compressible flows)
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AoA= 8.0
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%
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% Free-stream temperature (Rankine for US)
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FREESTREAM_TEMPERATURE= 518.67
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%
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% Reynolds number (non-dimensional, based on the free-stream values and ref MAC)
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REYNOLDS_NUMBER= 3.26E6
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%
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% Reynolds length (ref MAC of 275.8 inch)
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REYNOLDS_LENGTH= 275.80
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% ---------------------- REFERENCE VALUE DEFINITION ---------------------------%
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%
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% Reference origin for moment computation
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REF_ORIGIN_MOMENT_X = 1325.90
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REF_ORIGIN_MOMENT_Y = 0.0
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REF_ORIGIN_MOMENT_Z = 177.95
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%
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% Reference length for pitching, rolling, and yawing non-dimensional moment
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REF_LENGTH= 275.80
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%
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% Reference area for force coefficients (0 implies automatic calculation)
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REF_AREA= 297360.0
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%
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% Flow non-dimensionalization (DIMENSIONAL, FREESTREAM_PRESS_EQ_ONE,
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% FREESTREAM_VEL_EQ_MACH, FREESTREAM_VEL_EQ_ONE)
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REF_DIMENSIONALIZATION= FREESTREAM_PRESS_EQ_ONE
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% -------------------- BOUNDARY CONDITION DEFINITION --------------------------%
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%
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% Navier-Stokes wall boundary marker(s) (NONE = no marker)
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MARKER_HEATFLUX= (TRI_bdy2, 0.0, TRI_bdy5, 0.0, TRI_bdy7, 0.0, TRI_bdy9, 0.0, QUAD_bdy2, 0.0, QUAD_bdy5, 0.0, QUAD_bdy7, 0.0, QUAD_bdy9, 0.0, TRI_bdy3, 0.0, QUAD_bdy3, 0.0 )
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%
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% Farfield boundary marker(s) (NONE = no marker)
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MARKER_FAR= ( TRI_bdy1, TRI_bdy4, TRI_bdy6 )
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%
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% Symmetry boundary marker(s) (NONE = no marker)
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MARKER_SYM= ( TRI_bdy8, QUAD_bdy8 )
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%
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% Marker(s) of the surface to be plotted or designed
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MARKER_PLOTTING= (TRI_bdy2, TRI_bdy5, TRI_bdy7, TRI_bdy9, QUAD_bdy2, QUAD_bdy5, QUAD_bdy7, QUAD_bdy9, TRI_bdy3, QUAD_bdy3 )
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%
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% Marker(s) of the surface where the functional (Cd, Cl, etc.) will be evaluated
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MARKER_MONITORING= (TRI_bdy2, TRI_bdy5, TRI_bdy7, TRI_bdy9, QUAD_bdy2, QUAD_bdy5, QUAD_bdy7, QUAD_bdy9, TRI_bdy3, QUAD_bdy3)
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% ------------- COMMON PARAMETERS DEFINING THE NUMERICAL METHOD ---------------%
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%
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% Numerical method for spatial gradients (GREEN_GAUSS, WEIGHTED_LEAST_SQUARES)
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NUM_METHOD_GRAD= GREEN_GAUSS
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%
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% Courant-Friedrichs-Lewy condition of the finest grid
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CFL_NUMBER= 15.0
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%
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% Adaptive CFL number (NO, YES)
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CFL_ADAPT= YES
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%
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% Parameters of the adaptive CFL number (factor down, factor up, CFL min value,
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% CFL max value )
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CFL_ADAPT_PARAM= ( 1.5, 0.5, 15.0, 100.0 )
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%
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% Number of total iterations
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EXT_ITER= 30000
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% ----------------------- SLOPE LIMITER DEFINITION ----------------------------%
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%
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% Coefficient for the limiter
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VENKAT_LIMITER_COEFF= 0.05
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%
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% Coefficient for the sharp edges limiter
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ADJ_SHARP_LIMITER_COEFF= 3.0
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%
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% Reference coefficient (sensitivity) for detecting sharp edges.
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REF_SHARP_EDGES= 3.0
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%
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% Remove sharp edges from the sensitivity evaluation (NO, YES)
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SENS_REMOVE_SHARP= NO
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% ------------------------ LINEAR SOLVER DEFINITION ---------------------------%
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%
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% Linear solver for implicit formulations (BCGSTAB, FGMRES)
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LINEAR_SOLVER= FGMRES
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%
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% Preconditioner of the Krylov linear solver (JACOBI, LINELET, LU_SGS)
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LINEAR_SOLVER_PREC= ILU
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%
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% Linaer solver ILU preconditioner fill-in level (0 by default)
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LINEAR_SOLVER_ILU_FILL_IN= 0
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%
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% Minimum error of the linear solver for implicit formulations
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LINEAR_SOLVER_ERROR= 1E-10
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%
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% Max number of iterations of the linear solver for the implicit formulation
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LINEAR_SOLVER_ITER= 5
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% -------------------------- MULTIGRID PARAMETERS -----------------------------%
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%
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% Multi-grid levels (0 = no multi-grid)
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MGLEVEL= 0
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%
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% Multi-grid cycle (V_CYCLE, W_CYCLE, FULLMG_CYCLE)
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MGCYCLE= V_CYCLE
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%
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% Multi-grid pre-smoothing level
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MG_PRE_SMOOTH= ( 1, 2, 3, 3 )
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%
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% Multi-grid post-smoothing level
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MG_POST_SMOOTH= ( 0, 0, 0, 0 )
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%
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% Jacobi implicit smoothing of the correction
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MG_CORRECTION_SMOOTH= ( 0, 0, 0, 0 )
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%
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% Damping factor for the residual restriction
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MG_DAMP_RESTRICTION= 0.75
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%
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% Damping factor for the correction prolongation
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MG_DAMP_PROLONGATION= 0.75
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% -------------------- FLOW NUMERICAL METHOD DEFINITION -----------------------%
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%
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% Convective numerical method (JST, LAX-FRIEDRICH, CUSP, ROE, AUSM, HLLC,
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% TURKEL_PREC, MSW)
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CONV_NUM_METHOD_FLOW= ROE
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%
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% Monotonic Upwind Scheme for Conservation Laws (TVD) in the flow equations.
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% Required for 2nd order upwind schemes (NO, YES)
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MUSCL_FLOW= YES
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%
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% Slope limiter (VENKATAKRISHNAN, MINMOD)
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SLOPE_LIMITER_FLOW= VENKATAKRISHNAN
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%
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% Time discretization (RUNGE-KUTTA_EXPLICIT, EULER_IMPLICIT, EULER_EXPLICIT)
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TIME_DISCRE_FLOW= EULER_IMPLICIT
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%
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% Relaxation coefficient
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RELAXATION_FACTOR_FLOW= 0.9
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% -------------------- TURBULENT NUMERICAL METHOD DEFINITION ------------------%
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%
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% Convective numerical method (SCALAR_UPWIND)
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CONV_NUM_METHOD_TURB= SCALAR_UPWIND
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%
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% Monotonic Upwind Scheme for Conservation Laws (TVD) in the turbulence equations.
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% Required for 2nd order upwind schemes (NO, YES)
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MUSCL_TURB= NO
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%
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% Slope limiter (VENKATAKRISHNAN, MINMOD)
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SLOPE_LIMITER_TURB= VENKATAKRISHNAN
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%
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% Time discretization (EULER_IMPLICIT)
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TIME_DISCRE_TURB= EULER_IMPLICIT
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%
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% Relaxation coefficient
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RELAXATION_FACTOR_TURB= 0.9
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% --------------------------- CONVERGENCE PARAMETERS --------------------------%
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%
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% Convergence criteria (CAUCHY, RESIDUAL)
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CONV_CRITERIA= RESIDUAL
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%
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% Residual reduction (order of magnitude with respect to the initial value)
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RESIDUAL_REDUCTION= 6
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%
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% Min value of the residual (log10 of the residual)
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RESIDUAL_MINVAL= -12
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%
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% Start convergence criteria at iteration number
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STARTCONV_ITER= 10
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%
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% Number of elements to apply the criteria
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CAUCHY_ELEMS= 100
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%
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% Epsilon to control the series convergence
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CAUCHY_EPS= 1E-10
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%
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% Direct function to apply the convergence criteria (LIFT, DRAG, NEARFIELD_PRESS)
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CAUCHY_FUNC_FLOW= DRAG
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%
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% Adjoint function to apply the convergence criteria (SENS_GEOMETRY, SENS_MACH)
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CAUCHY_FUNC_ADJFLOW= SENS_GEOMETRY
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% ------------------------- INPUT/OUTPUT INFORMATION --------------------------%
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%
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% Mesh input file (Medium grid by default, same cfg file will work for Coarse)
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MESH_FILENAME= Woeber_Pointwise_HLCRM_FullGap_HexPrismPyrTets_Medium.cgns
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%MESH_FILENAME= Woeber_Pointwise_HLCRM_FullGap_HexPrismPyrTets_Coarse.cgns
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%
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% Mesh input file format (SU2, CGNS, NETCDF_ASCII)
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MESH_FORMAT= CGNS
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%
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% Mesh output file
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MESH_OUT_FILENAME= mesh_out.su2
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%
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% Restart flow input file
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SOLUTION_FLOW_FILENAME= solution_flow.dat
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%
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% Restart adjoint input file
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SOLUTION_ADJ_FILENAME= solution_adj.dat
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%
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% Output file format (TECPLOT, TECPLOT_BINARY, PARAVIEW,
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% FIELDVIEW, FIELDVIEW_BINARY)
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OUTPUT_FORMAT= PARAVIEW
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%
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% Output file convergence history (w/o extension)
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CONV_FILENAME= history
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%
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% Output file restart flow
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RESTART_FLOW_FILENAME= restart_flow.dat
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%
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% Output file restart adjoint
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RESTART_ADJ_FILENAME= restart_adj.dat
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%
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% Output file flow (w/o extension) variables
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VOLUME_FLOW_FILENAME= flow
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%
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% Output file adjoint (w/o extension) variables
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VOLUME_ADJ_FILENAME= adjoint
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%
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% Output objective function gradient (using continuous adjoint)
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GRAD_OBJFUNC_FILENAME= of_grad.dat
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%
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% Output file surface flow coefficient (w/o extension)
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SURFACE_FLOW_FILENAME= surface_flow
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%
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% Output file surface adjoint coefficient (w/o extension)
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SURFACE_ADJ_FILENAME= surface_adjoint
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%
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% Writing solution file frequency
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WRT_SOL_FREQ= 500
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%
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% Writing convergence history frequency
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WRT_CON_FREQ= 1
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%
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% Output residual values in the solution files
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WRT_RESIDUALS= NO
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%
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% Output limiters values in the solution files
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WRT_LIMITERS= NO
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%
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% Output the sharp edges detector
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WRT_SHARPEDGES= NO
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