|
| enum | SU2_COMPONENT {
SU2_CFD = 1,
SU2_DEF = 2,
SU2_DOT = 3,
SU2_MSH = 4,
SU2_GEO = 5,
SU2_SOL = 6
} |
| | different software components of SU2 More...
|
| |
| enum | ANSWER { NONE = 0,
NO = 0,
YES = 1
} |
| | Boolean answers. More...
|
| |
| enum | VERB_LEVEL { VERB_NONE = 0,
VERB_MEDIUM = 1,
VERB_HIGH = 2
} |
| | Verbosity level. More...
|
| |
| enum | ENUM_SOLVER {
NO_SOLVER = 0,
EULER = 1,
NAVIER_STOKES = 2,
RANS = 3,
POISSON_EQUATION = 4,
WAVE_EQUATION = 10,
HEAT_EQUATION = 29,
FLUID_STRUCTURE_INTERACTION = 12,
FEM_ELASTICITY = 13,
ADJ_EULER = 18,
ADJ_NAVIER_STOKES = 19,
ADJ_RANS = 20,
TEMPLATE_SOLVER = 30,
DISC_ADJ_EULER = 35,
DISC_ADJ_RANS = 36,
DISC_ADJ_NAVIER_STOKES = 37
} |
| | different solver types for the CFD component More...
|
| |
| enum | ENUM_FSI_FLUID_PROBLEM { NO_SOLVER_FFSI = 0,
EULER_FFSI = 1,
NAVIER_STOKES_FFSI = 2,
RANS_FFSI = 3
} |
| | types of fluid solvers More...
|
| |
| enum | ENUM_FSI_STRUC_PROBLEM { NO_SOLVER_SFSI = 0,
FEM_ELASTICITY_SFSI = 13
} |
| | types of structural solvers More...
|
| |
| enum | ENUM_STRUCT_SOLVER { SMALL_DEFORMATIONS = 0,
LARGE_DEFORMATIONS = 1
} |
| | Material geometric conditions. More...
|
| |
| enum | ENUM_MATERIAL_MODEL { LINEAR_ELASTIC = 0,
NEO_HOOKEAN = 1
} |
| | Material model. More...
|
| |
| enum | ENUM_MAT_COMPRESS { COMPRESSIBLE_MAT = 0,
INCOMPRESSIBLE_MAT = 1
} |
| | Material compressibility. More...
|
| |
| enum | ENUM_INTERPOLATOR { NEAREST_NEIGHBOR = 0,
ISOPARAMETRIC = 1,
CONSISTCONSERVE = 2
} |
| | types of interpolators More...
|
| |
| enum | ENUM_REGIME { COMPRESSIBLE = 0,
INCOMPRESSIBLE = 1
} |
| | different regime modes More...
|
| |
| enum | ENUM_KIND_NONDIM { DIMENSIONAL = 0,
FREESTREAM_PRESS_EQ_ONE = 1,
FREESTREAM_VEL_EQ_MACH = 2,
FREESTREAM_VEL_EQ_ONE = 3
} |
| | different non-dimensional modes More...
|
| |
| enum | ENUM_MEASUREMENTS { SI = 0,
US = 1
} |
| | different system of measurements More...
|
| |
| enum | RUNTIME_TYPE {
RUNTIME_FLOW_SYS = 2,
RUNTIME_TURB_SYS = 3,
RUNTIME_POISSON_SYS = 4,
RUNTIME_ADJPOT_SYS = 5,
RUNTIME_ADJFLOW_SYS = 6,
RUNTIME_ADJTURB_SYS = 7,
RUNTIME_WAVE_SYS = 8,
RUNTIME_MULTIGRID_SYS = 14,
RUNTIME_FEA_SYS = 20,
RUNTIME_HEAT_SYS = 21,
RUNTIME_TRANS_SYS = 22
} |
| | different types of systems More...
|
| |
| enum | ENUM_MATH_PROBLEM { DIRECT = 0,
CONTINUOUS_ADJOINT = 1,
DISCRETE_ADJOINT = 2
} |
| | types of mathematical problem to solve More...
|
| |
| enum | ENUM_SPACE { NO_CONVECTIVE = 0,
SPACE_CENTERED = 1,
SPACE_UPWIND = 2
} |
| | types of spatial discretizations More...
|
| |
| enum | ENUM_FLUIDMODEL { STANDARD_AIR = 0,
IDEAL_GAS = 1,
VW_GAS = 2,
PR_GAS = 3
} |
| | types of fluid model More...
|
| |
| enum | ENUM_INIT_OPTION { REYNOLDS = 0,
TD_CONDITIONS = 1
} |
| | types of initialization option More...
|
| |
| enum | ENUM_FREESTREAM_OPTION { TEMPERATURE_FS = 0,
DENSITY_FS = 1
} |
| | types of initialization option More...
|
| |
| enum | ENUM_VISCOSITYMODEL { CONSTANT_VISCOSITY = 0,
SUTHERLAND = 1
} |
| | types of viscosity model More...
|
| |
| enum | ENUM_CONDUCTIVITYMODEL { CONSTANT_CONDUCTIVITY = 0,
CONSTANT_PRANDTL = 1
} |
| | types of thermal conductivity model More...
|
| |
| enum | ENUM_GRIDMOVEMENT {
NO_MOVEMENT = 0,
DEFORMING = 1,
RIGID_MOTION = 2,
FLUID_STRUCTURE = 3,
EXTERNAL = 4,
EXTERNAL_ROTATION = 5,
AEROELASTIC = 6,
MOVING_WALL = 7,
ROTATING_FRAME = 8,
ELASTICITY = 9,
AEROELASTIC_RIGID_MOTION = 10,
STEADY_TRANSLATION = 11,
GUST = 12,
MOVING_HTP = 13
} |
| | types of unsteady mesh motion More...
|
| |
| enum | ENUM_GUST_TYPE {
NO_GUST = 0,
TOP_HAT = 1,
SINE = 2,
ONE_M_COSINE = 3,
VORTEX = 4,
EOG = 5
} |
| | type of wind gusts More...
|
| |
| enum | ENUM_GUST_DIR { X_DIR = 0,
Y_DIR = 1
} |
| | type of wind direction More...
|
| |
| enum | ENUM_CENTERED { NO_CENTERED = 0,
JST = 1,
LAX = 2,
JST_KE = 4
} |
| | types of centered spatial discretizations More...
|
| |
| enum | ENUM_UPWIND {
NO_UPWIND = 0,
ROE = 1,
SCALAR_UPWIND = 2,
AUSM = 3,
HLLC = 4,
SW = 5,
MSW = 6,
TURKEL = 7,
AUSMPWPLUS = 8,
CUSP = 9,
CONVECTIVE_TEMPLATE = 10
} |
| | types of upwind spatial discretizations More...
|
| |
| enum | ENUM_SPATIAL_ORDER { FIRST_ORDER = 0,
SECOND_ORDER = 1,
SECOND_ORDER_LIMITER = 2
} |
| | Spatial numerical order integration. More...
|
| |
| enum | ENUM_LIMITER { VENKATAKRISHNAN = 0,
BARTH_JESPERSEN = 1,
SHARP_EDGES = 2,
SOLID_WALL_DISTANCE = 3
} |
| | types of slope limiters More...
|
| |
| enum | ENUM_TURB_MODEL { NO_TURB_MODEL = 0,
SA = 1,
SA_NEG = 2,
SST = 3
} |
| | types of turbulent models More...
|
| |
| enum | ENUM_TRANS_MODEL { NO_TRANS_MODEL = 0,
LM = 1,
BC = 2
} |
| | types of transition models More...
|
| |
| enum | ENUM_TIME_INT { RUNGE_KUTTA_EXPLICIT = 1,
EULER_EXPLICIT = 2,
EULER_IMPLICIT = 3
} |
| | type of time integration schemes More...
|
| |
| enum | ENUM_TIME_INT_FEA { CD_EXPLICIT = 1,
NEWMARK_IMPLICIT = 2,
GENERALIZED_ALPHA = 3
} |
| | type of time integration schemes More...
|
| |
| enum | ENUM_SPACE_ITE_FEA { NEWTON_RAPHSON = 1,
MODIFIED_NEWTON_RAPHSON = 2
} |
| | type of time integration schemes More...
|
| |
| enum | ENUM_TRANSFER_METHOD { BROADCAST_DATA = 1,
SCATTER_DATA = 2,
ALLGATHER_DATA = 3,
LEGACY_METHOD = 4
} |
| | types of transfer methods More...
|
| |
| enum | ENUM_FLOW_GRADIENT { GREEN_GAUSS = 1,
WEIGHTED_LEAST_SQUARES = 2
} |
| | types of schemes to compute the flow gradient More...
|
| |
| enum | GEOMETRY_ACTION { ALLOCATE = 0,
UPDATE = 1
} |
| | types of action to take on a geometry structure More...
|
| |
| enum | GEOMETRY_MODE { FUNCTION = 0,
GRADIENT = 1
} |
| | types of action to perform when doing the geometry evaluation More...
|
| |
| enum | BC_TYPE {
EULER_WALL = 1,
FAR_FIELD = 2,
SYMMETRY_PLANE = 3,
INLET_FLOW = 4,
OUTLET_FLOW = 5,
PERIODIC_BOUNDARY = 6,
NEARFIELD_BOUNDARY = 7,
ELECTRODE_BOUNDARY = 8,
DIELEC_BOUNDARY = 9,
CUSTOM_BOUNDARY = 10,
INTERFACE_BOUNDARY = 11,
DIRICHLET = 12,
NEUMANN = 13,
DISPLACEMENT_BOUNDARY = 14,
LOAD_BOUNDARY = 15,
FLOWLOAD_BOUNDARY = 16,
SUPERSONIC_INLET = 19,
SUPERSONIC_OUTLET = 20,
ENGINE_INFLOW = 21,
ENGINE_EXHAUST = 22,
RIEMANN_BOUNDARY = 24,
ISOTHERMAL = 25,
HEAT_FLUX = 26,
PRESSURE_BOUNDARY = 27,
ACTDISK_INLET = 32,
ACTDISK_OUTLET = 33,
CLAMPED_BOUNDARY = 34,
LOAD_DIR_BOUNDARY = 35,
LOAD_SINE_BOUNDARY = 36,
NRBC_BOUNDARY = 37,
INTERNAL_BOUNDARY = 38,
FLUID_INTERFACE = 39,
SEND_RECEIVE = 99
} |
| | types of boundary conditions More...
|
| |
| enum | ENUM_2DFORM { PLANE_STRESS = 0,
PLANE_STRAIN = 1
} |
| | different regime modes More...
|
| |
| enum | ENUM_AITKEN { NO_RELAXATION = 0,
FIXED_PARAMETER = 1,
AITKEN_DYNAMIC = 2
} |
| | different regime modes More...
|
| |
| enum | RIEMANN_TYPE {
TOTAL_CONDITIONS_PT = 1,
DENSITY_VELOCITY = 2,
STATIC_PRESSURE = 3,
TOTAL_SUPERSONIC_INFLOW = 4,
STATIC_SUPERSONIC_INFLOW_PT = 5,
STATIC_SUPERSONIC_INFLOW_PD = 6,
MIXING_IN = 7,
MIXING_OUT = 8
} |
| | types Riemann boundary treatments More...
|
| |
| enum | MIXINGPROCESS_TYPE { ALGEBRAIC_AVERAGE = 1,
AREA_AVERAGE = 2,
MIXEDOUT_AVERAGE = 3
} |
| | types of mixing process for averaging quantities at the boundaries. More...
|
| |
| enum | TURBO_PERFORMANCE_TYPE { BLADE = 1,
STAGE = 2,
TURBINE = 3
} |
| | types of Turbomachinery performance indicators. More...
|
| |
| enum | INLET_TYPE { TOTAL_CONDITIONS = 1,
MASS_FLOW = 2,
INPUT_FILE = 3
} |
| | types inlet boundary treatments More...
|
| |
| enum | ENGINE_INFLOW_TYPE { FAN_FACE_MACH = 1,
FAN_FACE_MDOT = 2,
FAN_FACE_PRESSURE = 3
} |
| | types engine inflow boundary treatments More...
|
| |
| enum | ACTDISK_TYPE {
VARIABLES_JUMP = 1,
BC_THRUST = 2,
NET_THRUST = 3,
DRAG_MINUS_THRUST = 4,
MASSFLOW = 5,
POWER = 6
} |
| | types actuator disk boundary treatments More...
|
| |
| enum | GEO_TYPE {
VERTEX = 1,
LINE = 3,
TRIANGLE = 5,
QUADRILATERAL = 9,
TETRAHEDRON = 10,
HEXAHEDRON = 12,
PRISM = 13,
PYRAMID = 14
} |
| | types of geometric entities based on VTK nomenclature More...
|
| |
| enum | ENUM_OBJECTIVE {
DRAG_COEFFICIENT = 1,
LIFT_COEFFICIENT = 2,
SIDEFORCE_COEFFICIENT = 3,
EFFICIENCY = 4,
INVERSE_DESIGN_PRESSURE = 5,
INVERSE_DESIGN_HEATFLUX = 6,
TOTAL_HEATFLUX = 7,
MAXIMUM_HEATFLUX = 8,
MOMENT_X_COEFFICIENT = 9,
MOMENT_Y_COEFFICIENT = 10,
MOMENT_Z_COEFFICIENT = 11,
EQUIVALENT_AREA = 12,
NEARFIELD_PRESSURE = 13,
FORCE_X_COEFFICIENT = 14,
FORCE_Y_COEFFICIENT = 15,
FORCE_Z_COEFFICIENT = 16,
THRUST_COEFFICIENT = 17,
TORQUE_COEFFICIENT = 18,
FIGURE_OF_MERIT = 19,
MAX_THICKNESS = 21,
MIN_THICKNESS = 22,
MAX_THICK_SEC1 = 23,
MAX_THICK_SEC2 = 24,
MAX_THICK_SEC3 = 25,
MAX_THICK_SEC4 = 26,
MAX_THICK_SEC5 = 27,
AVG_TOTAL_PRESSURE = 28,
AVG_OUTLET_PRESSURE = 29,
MASS_FLOW_RATE = 30,
OUTFLOW_GENERALIZED = 31,
AERO_DRAG_COEFFICIENT = 35,
RADIAL_DISTORTION = 36,
CIRCUMFERENTIAL_DISTORTION = 37
} |
| | types of objective functions More...
|
| |
| enum | ENUM_RESIDUAL { RHO_RESIDUAL = 1,
RHO_ENERGY_RESIDUAL = 2
} |
| | types of residual criteria equations More...
|
| |
| enum | ENUM_SENS { SENS_GEOMETRY = 1,
SENS_MACH = 2,
SENS_AOA = 3,
SENS_AOS = 4
} |
| | types of sensitivities to compute More...
|
| |
| enum | ENUM_ADAPT {
NO_ADAPT = 0,
FULL = 1,
FULL_FLOW = 2,
FULL_ADJOINT = 3,
GRAD_FLOW = 5,
GRAD_ADJOINT = 6,
GRAD_FLOW_ADJ = 7,
COMPUTABLE = 9,
REMAINING = 10,
WAKE = 12,
SMOOTHING = 14,
SUPERSONIC_SHOCK = 15,
PERIODIC = 17
} |
| | types of grid adaptation/refinement More...
|
| |
| enum | ENUM_INPUT { SU2 = 1,
CGNS = 2
} |
| | types of input file formats More...
|
| |
| enum | ENUM_OUTPUT {
TECPLOT = 1,
TECPLOT_BINARY = 2,
FIELDVIEW = 3,
FIELDVIEW_BINARY = 4,
CSV = 5,
CGNS_SOL = 6,
PARAVIEW = 7
} |
| | type of solution output file formats More...
|
| |
| enum | JUMP_DEFINITION { DIFFERENCE = 1,
RATIO = 2
} |
| | type of jump definition More...
|
| |
| enum | MG_CYCLE { V_CYCLE = 0,
W_CYCLE = 1,
FULLMG_CYCLE = 2
} |
| | type of multigrid cycle More...
|
| |
| enum | ENUM_OUTPUT_VARS {
DENSITY = 1,
VEL_X = 2,
VEL_Y = 3,
VEL_Z = 4,
PRESSURE = 5,
MACH = 6,
TEMPERATURE = 7,
LAM_VISC = 8,
EDDY_VISC = 9
} |
| | type of solution output variables More...
|
| |
| enum | ENUM_PARAM {
TRANSLATION = 0,
ROTATION = 1,
SCALE = 2,
FFD_SETTING = 3,
FFD_CONTROL_POINT = 4,
FFD_NACELLE = 5,
FFD_GULL = 6,
FFD_CAMBER = 7,
FFD_TWIST = 8,
FFD_THICKNESS = 9,
FFD_DIHEDRAL_ANGLE = 10,
FFD_ROTATION = 11,
FFD_CONTROL_POINT_2D = 12,
FFD_CAMBER_2D = 13,
FFD_THICKNESS_2D = 14,
FFD_TWIST_2D = 15,
FFD_CONTROL_SURFACE = 16,
HICKS_HENNE = 17,
PARABOLIC = 18,
NACA_4DIGITS = 19,
AIRFOIL = 20,
CST = 21,
SURFACE_BUMP = 22,
SURFACE_FILE = 23,
CUSTOM = 24,
NO_DEFORMATION = 25,
ANGLE_OF_ATTACK = 101,
FFD_ANGLE_OF_ATTACK = 102
} |
| | types of design parameterizations More...
|
| |
| enum | ENUM_FFD_BLENDING { BSPLINE_UNIFORM = 0,
BEZIER = 1
} |
| | types of FFD Blending function
|
| |
| enum | ENUM_LINEAR_SOLVER {
STEEPEST_DESCENT = 1,
NEWTON = 2,
QUASI_NEWTON = 3,
CONJUGATE_GRADIENT = 4,
FGMRES = 5,
BCGSTAB = 6,
RESTARTED_FGMRES = 7,
SMOOTHER_LUSGS = 8,
SMOOTHER_JACOBI = 9,
SMOOTHER_ILU = 10,
SMOOTHER_LINELET = 11
} |
| | types of solvers for solving linear systems More...
|
| |
| enum | ENUM_FFD_CONTINUITY { DERIVATIVE_NONE = 0,
DERIVATIVE_1ST = 1,
DERIVATIVE_2ND = 2,
USER_INPUT = 3
} |
| | types surface continuity at the intersection with the FFD More...
|
| |
| enum | ENUM_FFD_COORD_SYSTEM { CARTESIAN = 0,
CYLINDRICAL = 1,
SPHERICAL = 2
} |
| | types of coordinates systems for the FFD
|
| |
| enum | ENUM_SENS_SMOOTHING { NO_SMOOTH = 0,
SOBOLEV = 1,
BIGRID = 2
} |
| | types of sensitivity smoothing More...
|
| |
| enum | ENUM_LINEAR_SOLVER_PREC { JACOBI = 1,
LU_SGS = 2,
LINELET = 3,
ILU = 4
} |
| | types of preconditioners for the linear solver More...
|
| |
| enum | ENUM_GEO_ANALYTIC {
NO_GEO_ANALYTIC = 0,
NACA0012_AIRFOIL = 1,
NACA4412_AIRFOIL = 2,
CYLINDER = 3,
BIPARABOLIC = 4
} |
| | types of analytic definitions for various geometries More...
|
| |
| enum | ENUM_AXIS_ORIENTATION { X_AXIS = 0,
Y_AXIS = 1,
Z_AXIS = 2
} |
| | types of axis orientation More...
|
| |
| enum | ENUM_UNSTEADY {
STEADY = 0,
TIME_STEPPING = 1,
DT_STEPPING_1ST = 2,
DT_STEPPING_2ND = 3,
ROTATIONAL_FRAME = 4,
HARMONIC_BALANCE = 5
} |
| | types of schemes for unsteady computations More...
|
| |
| enum | ENUM_CONVERGE_CRIT { CAUCHY = 1,
RESIDUAL = 2
} |
| | types of criteria to determine when the solution is converged More...
|
| |
| enum | ENUM_DEFORM_STIFFNESS { CONSTANT_STIFFNESS = 0,
INVERSE_VOLUME = 1,
WALL_DISTANCE = 2
} |
| | types of element stiffnesses imposed for FEA mesh deformation More...
|
| |
| enum | ENUM_DIRECTDIFF_VAR {
NO_DERIVATIVE = 0,
D_MACH = 1,
D_AOA = 2,
D_PRESSURE = 3,
D_TEMPERATURE = 4,
D_DENSITY = 5,
D_TURB2LAM = 6,
D_SIDESLIP = 7,
D_VISCOSITY = 8,
D_REYNOLDS = 9,
D_DESIGN = 10
} |
| | The direct differentation variables. More...
|
| |
| enum | ENUM_DYNAMIC { STATIC = 0,
DYNAMIC = 1
} |
| | types of schemes for dynamic structural computations More...
|
| |
|
|
const unsigned int | EXIT_DIVERGENCE = 2 |
| | Exit code (divergence).
|
| |
|
const unsigned int | BUFSIZE = 3000000 |
| | MPI buffer.
|
| |
|
const unsigned int | MAX_PARAMETERS = 10 |
| | Maximum number of parameters for a design variable definition.
|
| |
|
const unsigned int | MAX_NUMBER_PERIODIC = 10 |
| | Maximum number of periodic boundary conditions.
|
| |
|
const unsigned int | MAX_STRING_SIZE = 200 |
| | Maximum number of domains.
|
| |
|
const unsigned int | MAX_NUMBER_FFD = 10 |
| | Maximum number of FFDBoxes for the FFD.
|
| |
|
const unsigned int | MAX_SOLS = 6 |
| | Maximum number of solutions at the same time (dimension of solution container array).
|
| |
|
const unsigned int | MAX_TERMS = 6 |
| | Maximum number of terms in the numerical equations (dimension of solver container array).
|
| |
|
const unsigned int | MAX_ZONES = 3 |
| | Maximum number of zones.
|
| |
|
const unsigned int | MAX_FE_KINDS = 4 |
| | Maximum number of Finite Elements.
|
| |
|
const unsigned int | NO_RK_ITER = 0 |
| | No Runge-Kutta iteration.
|
| |
|
const unsigned int | OVERHEAD = 4 |
| | Overhead space above nMarker when allocating space for boundary elems (MPI + periodic).
|
| |
|
const unsigned int | MESH_0 = 0 |
| | Definition of the finest grid level.
|
| |
|
const unsigned int | MESH_1 = 1 |
| | Definition of the finest grid level.
|
| |
|
const unsigned int | ZONE_0 = 0 |
| | Definition of the first grid domain.
|
| |
|
const unsigned int | ZONE_1 = 1 |
| | Definition of the first grid domain.
|
| |
|
const su2double | STANDART_GRAVITY = 9.80665 |
| | Acceleration due to gravity at surface of earth.
|
| |
|
const su2double | EPS = 1.0E-16 |
| | Error scale.
|
| |
|
const su2double | TURB_EPS = 1.0E-16 |
| | Turbulent Error scale.
|
| |
|
const su2double | ONE2 = 0.5 |
| | One divided by two.
|
| |
|
const su2double | TWO3 = 2.0 / 3.0 |
| | Two divided by three.
|
| |
|
const su2double | FOUR3 = 4.0 / 3.0 |
| | Four divided by three.
|
| |
|
const su2double | PI_NUMBER = 4.0 * atan(1.0) |
| | Pi number.
|
| |
|
const int | MASTER_NODE = 0 |
| | Master node for MPI parallelization.
|
| |
|
const int | SINGLE_NODE = 1 |
| | There is only a node in the MPI parallelization.
|
| |
|
const int | SINGLE_ZONE = 1 |
| | There is only a zone.
|
| |
|
const unsigned short | N_ELEM_TYPES = 7 |
| | General output & CGNS defines.
|
| |
|
const unsigned short | N_POINTS_LINE = 2 |
| | General output & CGNS defines.
|
| |
|
const unsigned short | N_POINTS_TRIANGLE = 3 |
| | General output & CGNS defines.
|
| |
|
const unsigned short | N_POINTS_QUADRILATERAL = 4 |
| | General output & CGNS defines.
|
| |
|
const unsigned short | N_POINTS_TETRAHEDRON = 4 |
| | General output & CGNS defines.
|
| |
|
const unsigned short | N_POINTS_HEXAHEDRON = 8 |
| | General output & CGNS defines.
|
| |
|
const unsigned short | N_POINTS_PYRAMID = 5 |
| | General output & CGNS defines.
|
| |
|
const unsigned short | N_POINTS_PRISM = 6 |
| | General output & CGNS defines.
|
| |
|
const int | FLOW_SOL = 0 |
| | Position of the mean flow solution in the solver container array.
|
| |
|
const int | ADJFLOW_SOL = 1 |
| | Position of the continuous adjoint flow solution in the solver container array.
|
| |
|
const int | TURB_SOL = 2 |
| | Position of the turbulence model solution in the solver container array.
|
| |
|
const int | ADJTURB_SOL = 3 |
| | Position of the continuous adjoint turbulence solution in the solver container array.
|
| |
|
const int | TRANS_SOL = 4 |
| | Position of the transition model solution in the solver container array.
|
| |
|
const int | POISSON_SOL = 2 |
| | Position of the electronic potential solution in the solver container array.
|
| |
|
const int | WAVE_SOL = 1 |
| | Position of the wave equation in the solution solver array.
|
| |
|
const int | HEAT_SOL = 2 |
| | Position of the heat equation in the solution solver array.
|
| |
|
const int | FEA_SOL = 1 |
| | Position of the FEA equation in the solution solver array.
|
| |
|
const int | TEMPLATE_SOL = 0 |
| | Position of the template solution.
|
| |
|
const int | CONV_TERM = 0 |
| | Position of the convective terms in the numerics container array.
|
| |
|
const int | VISC_TERM = 1 |
| | Position of the viscous terms in the numerics container array.
|
| |
|
const int | SOURCE_FIRST_TERM = 2 |
| | Position of the first source term in the numerics container array.
|
| |
|
const int | SOURCE_SECOND_TERM = 3 |
| | Position of the second source term in the numerics container array.
|
| |
|
const int | CONV_BOUND_TERM = 4 |
| | Position of the convective boundary terms in the numerics container array.
|
| |
|
const int | VISC_BOUND_TERM = 5 |
| | Position of the viscous boundary terms in the numerics container array.
|
| |
|
const int | FEA_TERM = 0 |
| | Position of the finite element analysis terms in the numerics container array.
|
| |
| const int | EL_TRIA = 0 |
| | types of finite elements (in 2D or 3D) More...
|
| |
|
const int | EL_QUAD = 1 |
| | Elements of four nodes (2D).
|
| |
|
const int | EL_TETRA = 0 |
| | Elements of four nodes (3D).
|
| |
|
const int | EL_HEXA = 1 |
| | Elements of eight nodes (3D).
|
| |
|
const int | CGNS_STRING_SIZE = 33 |
| | Length of strings used in the CGNS format.
|
| |
Defines classes for referencing options for easy input in CConfig.
- Author
- J. Hicken, B. Tracey
- Version
- 5.0.0 "Raven"
Many of the classes in this file are templated, and therefore must be declared and defined here; to keep all elements together, there is no corresponding .cpp file at this time.
SU2 Original Developers: Dr. Francisco D. Palacios. Dr. Thomas D. Economon.
SU2 Developers: Prof. Juan J. Alonso's group at Stanford University. Prof. Piero Colonna's group at Delft University of Technology. Prof. Nicolas R. Gauger's group at Kaiserslautern University of Technology. Prof. Alberto Guardone's group at Polytechnic University of Milan. Prof. Rafael Palacios' group at Imperial College London. Prof. Edwin van der Weide's group at the University of Twente. Prof. Vincent Terrapon's group at the University of Liege.
Copyright (C) 2012-2017 SU2, the open-source CFD code.
SU2 is free software; you can redistribute it and/or modify it under the terms of the GNU Lesser General Public License as published by the Free Software Foundation; either version 2.1 of the License, or (at your option) any later version.
SU2 is distributed in the hope that it will be useful, but WITHOUT ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR A PARTICULAR PURPOSE. See the GNU Lesser General Public License for more details.
You should have received a copy of the GNU Lesser General Public License along with SU2. If not, see http://www.gnu.org/licenses/.