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glue-codes/openfast-cpp/5MW_Land_DLL_WTurb_cpp/5MW_Land_DLL_WTurb_cpp.fst
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| ------- OpenFAST EXAMPLE INPUT FILE ------------------------------------------- | ||
| FAST Certification Test #18: NREL 5.0 MW Baseline Wind Turbine (Onshore) | ||
| ---------------------- SIMULATION CONTROL -------------------------------------- | ||
| True Echo - Echo input data to <RootName>.ech (flag) | ||
| "FATAL" AbortLevel - Error level when simulation should abort (string) {"WARNING", "SEVERE", "FATAL"} | ||
| 60 TMax - Total run time (s) | ||
| 0.00625 DT - Recommended module time step (s) | ||
| 2 InterpOrder - Interpolation order for input/output time history (-) {1=linear, 2=quadratic} | ||
| 0 NumCrctn - Number of correction iterations (-) {0=explicit calculation, i.e., no corrections} | ||
| 99999 DT_UJac - Time between calls to get Jacobians (s) | ||
| 1E+06 UJacSclFact - Scaling factor used in Jacobians (-) | ||
| ---------------------- FEATURE SWITCHES AND FLAGS ------------------------------ | ||
| 1 CompElast - Compute structural dynamics (switch) {1=ElastoDyn; 2=ElastoDyn + BeamDyn for blades} | ||
| 1 CompInflow - Compute inflow wind velocities (switch) {0=still air; 1=InflowWind; 2=external from OpenFOAM} | ||
| 2 CompAero - Compute aerodynamic loads (switch) {0=None; 1=AeroDyn v14; 2=AeroDyn v15} | ||
| 1 CompServo - Compute control and electrical-drive dynamics (switch) {0=None; 1=ServoDyn} | ||
| 0 CompHydro - Compute hydrodynamic loads (switch) {0=None; 1=HydroDyn} | ||
| 0 CompSub - Compute sub-structural dynamics (switch) {0=None; 1=SubDyn; 2=External Platform MCKF} | ||
| 0 CompMooring - Compute mooring system (switch) {0=None; 1=MAP++; 2=FEAMooring; 3=MoorDyn; 4=OrcaFlex} | ||
| 0 CompIce - Compute ice loads (switch) {0=None; 1=IceFloe; 2=IceDyn} | ||
| ---------------------- INPUT FILES --------------------------------------------- | ||
| "NRELOffshrBsline5MW_Onshore_ElastoDyn.dat" EDFile - Name of file containing ElastoDyn input parameters (quoted string) | ||
| "../../openfast/5MW_Baseline/NRELOffshrBsline5MW_BeamDyn.dat" BDBldFile(1) - Name of file containing BeamDyn input parameters for blade 1 (quoted string) | ||
| "../../openfast/5MW_Baseline/NRELOffshrBsline5MW_BeamDyn.dat" BDBldFile(2) - Name of file containing BeamDyn input parameters for blade 2 (quoted string) | ||
| "../../openfast/5MW_Baseline/NRELOffshrBsline5MW_BeamDyn.dat" BDBldFile(3) - Name of file containing BeamDyn input parameters for blade 3 (quoted string) | ||
| "../../openfast/5MW_Baseline/NRELOffshrBsline5MW_InflowWind_12mps.dat" InflowFile - Name of file containing inflow wind input parameters (quoted string) | ||
| "NRELOffshrBsline5MW_Onshore_AeroDyn15.dat" AeroFile - Name of file containing aerodynamic input parameters (quoted string) | ||
| "NRELOffshrBsline5MW_Onshore_ServoDyn.dat" ServoFile - Name of file containing control and electrical-drive input parameters (quoted string) | ||
| "unused" HydroFile - Name of file containing hydrodynamic input parameters (quoted string) | ||
| "unused" SubFile - Name of file containing sub-structural input parameters (quoted string) | ||
| "unused" MooringFile - Name of file containing mooring system input parameters (quoted string) | ||
| "unused" IceFile - Name of file containing ice input parameters (quoted string) | ||
| ---------------------- OUTPUT -------------------------------------------------- | ||
| True SumPrint - Print summary data to "<RootName>.sum" (flag) | ||
| 5 SttsTime - Amount of time between screen status messages (s) | ||
| 99999 ChkptTime - Amount of time between creating checkpoint files for potential restart (s) | ||
| "default" DT_Out - Time step for tabular output (s) (or "default") | ||
| 0 TStart - Time to begin tabular output (s) | ||
| 0 OutFileFmt - Format for tabular (time-marching) output file (switch) {0: uncompressed binary [<RootName>.outb], 1: text file [<RootName>.out], 2: binary file [<RootName>.outb], 3: both 1 and 2} | ||
| True TabDelim - Use tab delimiters in text tabular output file? (flag) {uses spaces if false} | ||
| "ES10.3E2" OutFmt - Format used for text tabular output, excluding the time channel. Resulting field should be 10 characters. (quoted string) | ||
| ---------------------- LINEARIZATION ------------------------------------------- | ||
| False Linearize - Linearization analysis (flag) | ||
| False CalcSteady - Calculate a steady-state periodic operating point before linearization? [unused if Linearize=False] (flag) | ||
| 3 TrimCase - Controller parameter to be trimmed {1:yaw; 2:torque; 3:pitch} [used only if CalcSteady=True] (-) | ||
| 0.001 TrimTol - Tolerance for the rotational speed convergence [used only if CalcSteady=True] (-) | ||
| 0.01 TrimGain - Proportional gain for the rotational speed error (>0) [used only if CalcSteady=True] (rad/(rad/s) for yaw or pitch; Nm/(rad/s) for torque) | ||
| 0 Twr_Kdmp - Damping factor for the tower [used only if CalcSteady=True] (N/(m/s)) | ||
| 0 Bld_Kdmp - Damping factor for the blades [used only if CalcSteady=True] (N/(m/s)) | ||
| 2 NLinTimes - Number of times to linearize (-) [>=1] [unused if Linearize=False] | ||
| 30, 60 LinTimes - List of times at which to linearize (s) [1 to NLinTimes] [used only when Linearize=True and CalcSteady=False] | ||
| 1 LinInputs - Inputs included in linearization (switch) {0=none; 1=standard; 2=all module inputs (debug)} [unused if Linearize=False] | ||
| 1 LinOutputs - Outputs included in linearization (switch) {0=none; 1=from OutList(s); 2=all module outputs (debug)} [unused if Linearize=False] | ||
| False LinOutJac - Include full Jacobians in linearization output (for debug) (flag) [unused if Linearize=False; used only if LinInputs=LinOutputs=2] | ||
| False LinOutMod - Write module-level linearization output files in addition to output for full system? (flag) [unused if Linearize=False] | ||
| ---------------------- VISUALIZATION ------------------------------------------ | ||
| 0 WrVTK - VTK visualization data output: (switch) {0=none; 1=initialization data only; 2=animation; 3=mode shapes} | ||
| 1 VTK_type - Type of VTK visualization data: (switch) {1=surfaces; 2=basic meshes (lines/points); 3=all meshes (debug)} [unused if WrVTK=0] | ||
| true VTK_fields - Write mesh fields to VTK data files? (flag) {true/false} [unused if WrVTK=0] | ||
| 15 VTK_fps - Frame rate for VTK output (frames per second){will use closest integer multiple of DT} [used only if WrVTK=2 or WrVTK=3] |
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glue-codes/openfast-cpp/5MW_Land_DLL_WTurb_cpp/NRELOffshrBsline5MW_Onshore_AeroDyn15.dat
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| ------- AERODYN v15 for OpenFAST INPUT FILE ----------------------------------------------- | ||
| NREL 5.0 MW offshore baseline aerodynamic input properties. | ||
| ====== General Options ============================================================================ | ||
| False Echo - Echo the input to "<rootname>.AD.ech"? (flag) | ||
| "default" DTAero - Time interval for aerodynamic calculations {or "default"} (s) | ||
| 1 WakeMod - Type of wake/induction model (switch) {0=none, 1=BEMT, 2=DBEMT, 3=OLAF} [WakeMod cannot be 2 or 3 when linearizing] | ||
| 2 AFAeroMod - Type of blade airfoil aerodynamics model (switch) {1=steady model, 2=Beddoes-Leishman unsteady model} [AFAeroMod must be 1 when linearizing] | ||
| 1 TwrPotent - Type tower influence on wind based on potential flow around the tower (switch) {0=none, 1=baseline potential flow, 2=potential flow with Bak correction} | ||
| 0 TwrShadow - Calculate tower influence on wind based on downstream tower shadow (switch) {0=none, 1=Powles model, 2=Eames model} | ||
| True TwrAero - Calculate tower aerodynamic loads? (flag) | ||
| False FrozenWake - Assume frozen wake during linearization? (flag) [used only when WakeMod=1 and when linearizing] | ||
| False CavitCheck - Perform cavitation check? (flag) [AFAeroMod must be 1 when CavitCheck=true] | ||
| False CompAA - Flag to compute AeroAcoustics calculation [used only when WakeMod = 1 or 2] | ||
| "unused" AA_InputFile - AeroAcoustics input file [used only when CompAA=true] | ||
| ====== Environmental Conditions =================================================================== | ||
| 1.225 AirDens - Air density (kg/m^3) | ||
| 1.464E-05 KinVisc - Kinematic air viscosity (m^2/s) | ||
| 335 SpdSound - Speed of sound (m/s) | ||
| 103500 Patm - Atmospheric pressure (Pa) [used only when CavitCheck=True] | ||
| 1700 Pvap - Vapour pressure of fluid (Pa) [used only when CavitCheck=True] | ||
| 0.5 FluidDepth - Water depth above mid-hub height (m) [used only when CavitCheck=True] | ||
| ====== Blade-Element/Momentum Theory Options ====================================================== [unused when WakeMod=0 or 3] | ||
| 2 SkewMod - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [unused when WakeMod=0 or 3] | ||
| "default" SkewModFactor - Constant used in Pitt/Peters skewed wake model {or "default" is 15/32*pi} (-) [used only when SkewMod=2; unused when WakeMod=0 or 3] | ||
| True TipLoss - Use the Prandtl tip-loss model? (flag) [unused when WakeMod=0 or 3] | ||
| True HubLoss - Use the Prandtl hub-loss model? (flag) [unused when WakeMod=0 or 3] | ||
| True TanInd - Include tangential induction in BEMT calculations? (flag) [unused when WakeMod=0 or 3] | ||
| False AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod=0 or 3] | ||
| False TIDrag - Include the drag term in the tangential-induction calculation? (flag) [unused when WakeMod=0,3 or TanInd=FALSE] | ||
| "Default" IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [unused when WakeMod=0 or 3] | ||
| 100 MaxIter - Maximum number of iteration steps (-) [unused when WakeMod=0] | ||
| ====== Dynamic Blade-Element/Momentum Theory Options ============================================== [used only when WakeMod=2] | ||
| 2 DBEMT_Mod - Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2] | ||
| 4 tau1_const - Time constant for DBEMT (s) [used only when WakeMod=2 and DBEMT_Mod=1] | ||
| ====== OLAF -- cOnvecting LAgrangian Filaments (Free Vortex Wake) Theory Options ================== [used only when WakeMod=3] | ||
| "unused" OLAFInputFileName - Input file for OLAF [used only when WakeMod=3] | ||
| ====== Beddoes-Leishman Unsteady Airfoil Aerodynamics Options ===================================== [used only when AFAeroMod=2] | ||
| 3 UAMod - Unsteady Aero Model Switch (switch) {1=Baseline model (Original), 2=Gonzalez's variant (changes in Cn,Cc,Cm), 3=Minnema/Pierce variant (changes in Cc and Cm)} [used only when AFAeroMod=2] | ||
| True FLookup - Flag to indicate whether a lookup for f' will be calculated (TRUE) or whether best-fit exponential equations will be used (FALSE); if FALSE S1-S4 must be provided in airfoil input files (flag) [used only when AFAeroMod=2] | ||
| ====== Airfoil Information ========================================================================= | ||
| 1 AFTabMod - Interpolation method for multiple airfoil tables {1=1D interpolation on AoA (first table only); 2=2D interpolation on AoA and Re; 3=2D interpolation on AoA and UserProp} (-) | ||
| 1 InCol_Alfa - The column in the airfoil tables that contains the angle of attack (-) | ||
| 2 InCol_Cl - The column in the airfoil tables that contains the lift coefficient (-) | ||
| 3 InCol_Cd - The column in the airfoil tables that contains the drag coefficient (-) | ||
| 4 InCol_Cm - The column in the airfoil tables that contains the pitching-moment coefficient; use zero if there is no Cm column (-) | ||
| 0 InCol_Cpmin - The column in the airfoil tables that contains the Cpmin coefficient; use zero if there is no Cpmin column (-) | ||
| 8 NumAFfiles - Number of airfoil files used (-) | ||
| "../../openfast/5MW_Baseline/Airfoils/Cylinder1.dat" AFNames - Airfoil file names (NumAFfiles lines) (quoted strings) | ||
| "../../openfast/5MW_Baseline/Airfoils/Cylinder2.dat" | ||
| "../../openfast/5MW_Baseline/Airfoils/DU40_A17.dat" | ||
| "../../openfast/5MW_Baseline/Airfoils/DU35_A17.dat" | ||
| "../../openfast/5MW_Baseline/Airfoils/DU30_A17.dat" | ||
| "../../openfast/5MW_Baseline/Airfoils/DU25_A17.dat" | ||
| "../../openfast/5MW_Baseline/Airfoils/DU21_A17.dat" | ||
| "../../openfast/5MW_Baseline/Airfoils/NACA64_A17.dat" | ||
| ====== Rotor/Blade Properties ===================================================================== | ||
| True UseBlCm - Include aerodynamic pitching moment in calculations? (flag) | ||
| "../../openfast/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-) | ||
| "../../openfast/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2] | ||
| "../../openfast/5MW_Baseline/NRELOffshrBsline5MW_AeroDyn_blade.dat" ADBlFile(3) - Name of file containing distributed aerodynamic properties for Blade #3 (-) [unused if NumBl < 3] | ||
| ====== Tower Influence and Aerodynamics ============================================================= [used only when TwrPotent/=0, TwrShadow/=0, or TwrAero=True] | ||
| 12 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow/=0, or TwrAero=True] | ||
| TwrElev TwrDiam TwrCd TwrTI (used only with TwrShadow=2) | ||
| (m) (m) (-) (-) | ||
| 0.0000000E+00 6.0000000E+00 1.0000000E+00 1.0000000E-01 | ||
| 8.5261000E+00 5.7870000E+00 1.0000000E+00 1.0000000E-01 | ||
| 1.7053000E+01 5.5740000E+00 1.0000000E+00 1.0000000E-01 | ||
| 2.5579000E+01 5.3610000E+00 1.0000000E+00 1.0000000E-01 | ||
| 3.4105000E+01 5.1480000E+00 1.0000000E+00 1.0000000E-01 | ||
| 4.2633000E+01 4.9350000E+00 1.0000000E+00 1.0000000E-01 | ||
| 5.1158000E+01 4.7220000E+00 1.0000000E+00 1.0000000E-01 | ||
| 5.9685000E+01 4.5090000E+00 1.0000000E+00 1.0000000E-01 | ||
| 6.8211000E+01 4.2960000E+00 1.0000000E+00 1.0000000E-01 | ||
| 7.6738000E+01 4.0830000E+00 1.0000000E+00 1.0000000E-01 | ||
| 8.5268000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 | ||
| 8.7600000E+01 3.8700000E+00 1.0000000E+00 1.0000000E-01 | ||
| ====== Outputs ==================================================================================== | ||
| True SumPrint - Generate a summary file listing input options and interpolated properties to "<rootname>.AD.sum"? (flag) | ||
| 0 NBlOuts - Number of blade node outputs [0 - 9] (-) | ||
| 1, 9, 19 BlOutNd - Blade nodes whose values will be output (-) | ||
| 0 NTwOuts - Number of tower node outputs [0 - 9] (-) | ||
| 1, 2, 6 TwOutNd - Tower nodes whose values will be output (-) | ||
| OutList - The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-) | ||
| END of input file (the word "END" must appear in the first 3 columns of this last OutList line) | ||
| --------------------------------------------------------------------------------------- |
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