src

datastr.c File Reference

Detailed Description


Variables

const int _ntags = 124
const int _obsolete_ntags = 9
const tag _obsolete_taglist []
const tag _taglist []
double adc = 0.0
int ADC_iter = 0
double AERODYNAMIC [10]
double airfoil_Ia
double airfoil_Ib
double airfoil_Kaa
double airfoil_Kah = 0.0
double airfoil_Kbb
double airfoil_Kha = 0.0
double airfoil_Khh
double airfoil_m
double airfoil_Sa
double airfoil_Sab
double airfoil_Sb
char airfoilfile [FILENAME_LENGTH]
int ALE_CONSERVATIVE = 1
double * ALE_GridVelocityVector = NULL
int ALE_USE_DIVGRID = 1
vector ALEDeflection
sparse ALEGridMotion_Preconditioner
sparse ALEGridMotion_Stiffness
vector ALETension
double amplitude0 = 0.0
double amplitude1
double amplitude2
double amplitude3
double angle = 0.0
double angularvelocity = 0.0
int * base_pressure_idx = NULL
double ** basefn_values = NULL
vector bc
vector bc_p
vector bc_u
vector bc_v
long * BELE [2]
basefunction Bj
basefunction Bk
long BndrEdges [MAX_BOUNDARIES]
int BndrId [MAX_BOUNDARIES]
short ** BndrSideBsDescr = NULL
long ** BndrSideBsIdx = NULL
int BndrTypes = 0
long * BSIDE_INDEX = NULL
char cfgfile [FILENAME_LENGTH]
char coarsegridbasename [FILENAME_LENGTH]
double cofgheight = 0.0
double conservativity
int COUPLED_MODEL = 10
double CPDOWN_CoefA [21]
double CPDOWN_CoefB [21]
long CPDOWN_IDXA [21]
long CPDOWN_IDXB [21]
double CPUP_CoefA [21]
double CPUP_CoefB [21]
long CPUP_IDXA [21]
long CPUP_IDXB [21]
double current_time = 0.0
double damping_aa
double damping_ah = 0.0
double damping_bb
double damping_ha = 0.0
double damping_hh
int deg_bubble = 2
int deg_max = 2
int deg_press_bubble = 1
int deg_press_side = 1
int deg_side = 2
short * degx = NULL
short * degx_press = NULL
short * degy = NULL
short * degy_press = NULL
double delta = 0.0
double density = 1.225
double dissipation
vector DIST
double DragForce [HISTORY_LIFT]
long ** ELEMENT = NULL
long ** ELEMENT_BOUNDARY_SIDES = NULL
short * ELEMENT_MARK = NULL
int element_type = 1
short ** ElementBsDescr = NULL
long ** ElementBsIdx = NULL
int EMPLOYED_STABILIZATION = SUPG_STABILIZATION
basefunction EPS1
basefunction EPS2
double epsilon = 1e-12
double epsilon_abs = 1e-15
double epsilon_inner = 1e-10
double epsilon_newton = 1e-5
double epsilon_nonlinear = 1e-5
double epsilon_nonlinear_rel = 1e-5
double epsilon_ode = 1e-12
double epsilontime = 1e-10
double ** export_basefn_values
long FE_Dimension = 0
vector FiniteVolumeValues1
vector FiniteVolumeValues2
vector FiniteVolumeValues3
vector FiniteVolumeValues4
vector FiniteVolumeValues5
vector FiniteVolumeValues6
vector FiniteVolumeValues7
vector FiniteVolumeValues8
double FirstLayerDistance
long FixPressureIdx
double FlapTorsionalMoment [HISTORY_LIFT]
double fluid_density = 1.225
int FLUID_MODEL = 10
double fluid_viscosity = 1e-5
double force_lift
double force_moment
char forcesfile [FILENAME_LENGTH]
double freesurf_x0 = 0.0
double freesurf_x1 = 10.0
double freesurf_y0 = 0.6
double freesurf_y1 = 1.6
double frequency1
double frequency2
double frequency3
double gas_density = 1
double gas_viscosity = 1e-5
double global_bnorm = 1.0
long GMRESrestart = 4000
double ** grad_basefn_values [3]
char gridbasename [FILENAME_LENGTH]
double * GTension = NULL
double * GVel1 = NULL
double * GVel2 = NULL
double ** hes_basefn_values [3][3]
double inlet_velocity = 1.0
char iter_file [FILENAME_LENGTH]
long itime = 0
basefunction K1
basefunction K2
vector KEPS_eps0
vector KEPS_eps1
vector KEPS_eps2
vector KEPS_k0
vector KEPS_k1
vector KEPS_k2
double kinematic_viscosity = 1.5e-5
double kinetic_energy
double ** L = NULL
double ** L1 = NULL
double LiftForce [HISTORY_LIFT]
sparse LinSolS
vector LinValues1
vector LinValues2
vector LinValues3
long ListOfMatrixOutput [LIST_MAXLENGTH]
long * ListOfSidesFluidGas
long * ListofSidesFluidStructure
int LOAD_PROGRAM_STATE = 0
vector LocalLinValues1
vector LocalLinValues2
vector LocalLinValues3
vector locKX
vector locKY
vector locUX
vector locUY
vector locVX
vector locVY
char log_file [FILENAME_LENGTH]
matrix M
double max_side = 0.0
long MaxOfFSIter = 5
long MaxOfIter = 1000
long MaxOfIter_inner = 500
long MaxOfIterTime = 200
long MaxOfNonlinear = 50
double min_side = 1000.0
matrix Minv
int N1 = 0
int n1 = 0
int N2 = 0
int n2 = 0
long NBSides = 0
vector NDensityFunction
long NElements = 0
long NInterfaceFluidGas
long NInterfaceFluidStructure
vector NLevelSetFunction0
vector NLevelSetFunction1
vector NLevelSetFunction2
vector NLevelSetFunctionTMP
short * NodeBsDescr = NULL
long * NodeBsIdx = NULL
int NONLINEAR_STRUCTURE_MODEL = 1
double NONNEWTONIAN_POWER
double NONNEWTONIAN_VISCOSITY
long NPoints = 0
long NSides = 0
basefunction NUT
vector NViscosityFunction
basefunction OMG1
basefunction OMG2
int ONsavebinary = 2
int ONsavegmvoutput = 0
int ONsavepressureoutput = 1
int ONsaveresultsoutput = 0
int ONsavetecplotoutput = 1
int ONsavetecplotoutput1 = 0
long * PatchList = NULL
long * PatchW = NULL
short * PointMark
double prefIN0 = 0.0
double prefIN1 = 0.0
double prefIN2 = 0.0
double prefIN3 = 0.0
double prefIN4 = 0.0
double prefOUT = 0.0
short ** Pressure_BndrSideBsDescr = NULL
long ** Pressure_BndrSideBsIdx = NULL
short ** Pressure_ElementBsDescr = NULL
long ** Pressure_ElementBsIdx = NULL
long Pressure_FE_Dimension = 0
short * Pressure_NodeBsDescr = NULL
long * Pressure_NodeBsIdx = NULL
short ** Pressure_SideBsDescr = NULL
long ** Pressure_SideBsIdx = NULL
char pressurefile [FILENAME_LENGTH]
int Q1 = 0
int q1 = 0
int Q2 = 0
int q2 = 0
double * RecentGVel1 = NULL
double * RecentGVel2 = NULL
vector ref
double ref_L = 1.0
double ref_U = 1.0
double ref_W = 0.05
int RefDimBubble = 0
int RefDimSide = 0
double reference_PRESSURE0 = 0.0
double reference_PRESSURE1 = 0.0
double reference_PRESSURE2 = 0.0
double reference_PRESSURE3 = 0.0
double reference_PRESSURE4 = 0.0
double reference_PRESSURE_OUT = 0.0
int RefPressureDimBubble = 0
int RefPressureDimSide = 0
int RefPressureTriDim = 3
int RefTriDim = 3
char releasefile [FILENAME_LENGTH]
double releasetime = 5.0
double releasetimesec = 0.01
char report_file [FILENAME_LENGTH]
char rereadfile [FILENAME_LENGTH]
double restartangle = 0.0
double restartflap = 0.0
double restarty = 0.0
char results_file [FILENAME_LENGTH]
double Reynolds = 300.0
double * rh = NULL
double rho = 0.0
vector rhs
int saveevery = 1
int saveevery_inner = 1
int saveevery_pressure = 1
int saveeverytime = 1
long ** SIDE = NULL
short * SIDE_MARK = NULL
double * SIDE_S = NULL
double ** sidebasefn_values = NULL
short ** SideBsDescr = NULL
long ** SideBsIdx = NULL
double sigma = 0.0
double SOLVER_NONLINEAR [3]
long SOLVER_NONLINEAR_ITER
long SOLVER_NONLINEAR_TIME
void * SolverControl = NULL
void * SolverInfo = NULL
void * SolverNumeric
sparse SolverS
void * SolverSymbolic
vector SST_k0
vector SST_k1
vector SST_k2
vector SST_omg0
vector SST_omg1
vector SST_omg2
int STABILIZATION_CHOICE_DELTA = 0
int STABILIZATION_CHOICE_H = 1
int STABILIZATION_CHOICE_NORM = 2
char start [FILENAME_LENGTH]
char startlinear [FILENAME_LENGTH]
long STATIONARY_ITER = 0
char stop [FILENAME_LENGTH]
double structure_density = 1
int STRUCTURE_MODEL = 10
double SurfaceAverageHeight
char surfacefile [FILENAME_LENGTH]
double SurfaceLeft
double SurfaceMaxHeight
double SurfaceMinHeight
double SurfaceRight
double tail_angle = 0.0
double tau = 0.01
double theta_relaxation = 1.0
double TIME_PERIOD = 2.0
double time_physical
char timesol [FILENAME_LENGTH]
double TorsionalMoment [HISTORY_LIFT]
basefunction TRB1
basefunction TRB2
long triplet_allocated = 0
long * triplet_I
long * triplet_J
long triplet_nz = 0
double * triplet_VAL
long TurbulenceINNER = 1
double TWOPHASEKineticEnergy
double TWOPHASEMass
double TWOPHASEPotentialEnergy
motion U0
motion U1
motion U2
long * UsePatch = NULL
vector uvec0
vector uvec1
vector uvec2
vector uvectemp
vector valueA_Dx
vector valueA_Dy
vector valueB_Dx
vector valueB_Dy
double velocity_tailangle = 0.0
vector velU_Dx
vector velU_Dy
vector velV_Dx
vector velV_Dy
double visc_laminar = 1.0/300.0
vector visc_RANS
vector visc_SA0
vector visc_SA1
vector visc_SA2
vector visc_SATMP
double viscosity = 1.0/300.0
double * W = NULL
double * w = NULL
double * W2 = NULL
double * w2 = NULL
vector WALLdistance
motion WW
double * X = NULL
double * x = NULL
double * X1 = NULL
double * xh = NULL
double xhc
double xlast [HISTORY_LIFT][10]
double xmcenter
double xRECENT [10]
double * xT1 = NULL
double * xT2 = NULL
double xTAIL1 = 0.8
double xTAIL1orig = 0.8
double xTAIL2 = 0.81
double xTAIL2orig = 0.81
double * y = NULL
double * yh = NULL
double yhc
double YIELDSTRESS
double ymcenter
double * yT1 = NULL
double * yT2 = NULL
double yTAIL = 0.0
double yTAILorig = 0.0
double yvelocity = 0.0

Variable Documentation

const tag _taglist[]
 

TAG list - list of keywords in configuration file Describes how the configuration file should be read, list of TAGS(key-word,pointer,data-type)

const int _ntags = 124
 

Number of TAGS in _TAGLIST - configuration

const tag _obsolete_taglist[]
 

Initial value:

{       
    { "airfoiltorsionalfirstmoment=","RENAMED: airfoil torsional static moment",TAG_DOUBLE},
    { "airfoiltorsionalsecondmoment=","RENAMED: airfoil torsional inertia moment",TAG_DOUBLE},
    { "fluidmodel=","DELETED: now in coupled model",TAG_INT},          
    { "structuralmodel=","DELETED: now in coupled model",TAG_INT},     
    { "aleradius1=","N/A - not needed",TAG_DOUBLE},
    { "aleradius2=","N/A - not needed",TAG_DOUBLE},
    { "adsstabilization=","RENAMED: adc stabilization",TAG_DOUBLE},
    { "stokesfile=","N/A - not needed",TAG_DOUBLE},
    { "maximumoftimeiterations=","DELETED: now, compute from TIME PERIOD",TAG_LONG}
}
TAG list - obsolete TAGS - removed/renamed TAGS from TAGLIST Old/Unused TAGS in taglist

const int _obsolete_ntags = 9
 

Number of old TAGS in taglist

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