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Added OF2 files to NALU folder (see #4)
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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -0,0 +1,90 @@ | ||
| ------- AERODYN v15.04.* INPUT FILE ------------------------------------------------ | ||
| SNLV27 - v1 - OpenFAST | ||
| ====== General Options ============================================================================ | ||
| False Echo - Echo the input to "<rootname>.AD.ech"? (flag) | ||
| "default" DTAero - Time interval for aerodynamic calculations {or "default"} (s) | ||
| 0 WakeMod - Type of wake/induction model (switch) {0=none, 1=BEMT} | ||
| 2 AFAeroMod - Type of blade airfoil aerodynamics model (switch) {1=steady model, 2=Beddoes-Leishman unsteady model} | ||
| 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} | ||
| False TwrShadow - Calculate tower influence on wind based on downstream tower shadow? (flag) | ||
| 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) | ||
| ====== Environmental Conditions =================================================================== | ||
| 1.064032027823 AirDens - Air density (kg/m^3) | ||
| 1.5e-05 KinVisc - Kinematic air viscosity (m^2/s) | ||
| 335 SpdSound - Speed of sound (m/s) | ||
| 9999.9 Patm - Atmospheric pressure (Pa) [used only when CavitCheck=True] | ||
| 9999.9 Pvap - Vapour pressure of fluid (Pa) [used only when CavitCheck=True] | ||
| 9999.9 FluidDepth - Water depth above mid-hub height (m) [used only when CavitCheck=True] | ||
| ====== Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=1] | ||
| 2 SkewMod - Type of skewed-wake correction model (switch) {1=uncoupled, 2=Pitt/Peters, 3=coupled} [used only when WakeMod=1] | ||
| "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] | ||
| True TipLoss - Use the Prandtl tip-loss model? (flag) [used only when WakeMod=1] | ||
| True HubLoss - Use the Prandtl hub-loss model? (flag) [used only when WakeMod=1] | ||
| True TanInd - Include tangential induction in BEMT calculations? (flag) [used only when WakeMod=1] | ||
| False AIDrag - Include the drag term in the axial-induction calculation? (flag) [used only when WakeMod=1] | ||
| False TIDrag - Include the drag term in the tangential-induction calculation? (flag) [used only when WakeMod=1 and TanInd=TRUE] | ||
| "default" IndToler - Convergence tolerance for BEMT nonlinear solve residual equation {or "default"} (-) [used only when WakeMod=1] | ||
| 100 MaxIter - Maximum number of iteration steps (-) [used only when WakeMod=1] | ||
| ====== 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] | ||
| ====== 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=Minemma/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 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 (-) | ||
| 5 NumAFfiles - Number of airfoil files used (-) | ||
| "AeroData_AD15/AD_1_Cylinder.dat" AFNames - Airfoil file names (NumAFfiles lines) (quoted strings) | ||
| "AeroData_AD15/AD_2_63-235_mod.dat" | ||
| "AeroData_AD15/AD_3_63-224_mod.dat" | ||
| "AeroData_AD15/AD_4_63-218_mod.dat" | ||
| "AeroData_AD15/AD_5_63-214_mod.dat" | ||
| ====== Rotor/Blade Properties ===================================================================== | ||
| True UseBlCm - Include aerodynamic pitching moment in calculations? (flag) | ||
| "SNLV27_AeroDyn_Blade.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-) | ||
| "SNLV27_AeroDyn_Blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2] | ||
| "SNLV27_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=True, or TwrAero=True] | ||
| 12 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True] | ||
| TwrElev TwrDiam TwrCd | ||
| (m) (m) (-) | ||
| 0.0001000E+00 2.400000E+00 1.0000000E+00 | ||
| 3.0172272E+00 2.372367E+00 1.0000000E+00 | ||
| 6.0347374E+00 2.271293E+00 1.0000000E+00 | ||
| 9.0519292E+00 2.170254E+00 1.0000000E+00 | ||
| 1.2069121E+01 2.069226E+00 1.0000000E+00 | ||
| 1.5087021E+01 1.968187E+00 1.0000000E+00 | ||
| 1.8103858E+01 1.867172E+00 1.0000000E+00 | ||
| 2.1121404E+01 1.766121E+00 1.0000000E+00 | ||
| 2.4138596E+01 1.665094E+00 1.0000000E+00 | ||
| 2.7156142E+01 1.564066E+00 1.0000000E+00 | ||
| 3.0174749E+01 1.463028E+00 1.0000000E+00 | ||
| 3.1000000E+01 1.362000E+00 1.0000000E+00 | ||
| ====== Outputs ==================================================================================== | ||
| False 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, 20 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, (-) | ||
| RtTSR, | ||
| RtAeroCp | ||
| RtAeroCt | ||
| RtAeroFxh | ||
| RtAeroFyh | ||
| RtAeroFzh | ||
| RtAeroMxh | ||
| RtAeroMyh | ||
| RtAeroMzh | ||
| RtVAvgxh | ||
| RtVAvgyh | ||
| RtVAvgzh | ||
| RtArea | ||
| END of input file (the word "END" must appear in the first 3 columns of this last OutList line) | ||
| --------------------------------------------------------------------------------------- |
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| Original file line number | Diff line number | Diff line change |
|---|---|---|
| @@ -0,0 +1,54 @@ | ||
| ------- OpenFAST2 INPUT FILE ------------------------------------------------ | ||
| SNLV27 - v1 - OpenFAST2 | ||
| ---------------------- SIMULATION CONTROL -------------------------------------- | ||
| False Echo - Echo input data to <RootName>.ech (flag) | ||
| "FATAL" AbortLevel - Error level when simulation should abort (string) {"WARNING", "SEVERE", "FATAL"} | ||
| 2000 TMax - Total run time (s) | ||
| 0.005 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} | ||
| 2 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} | ||
| 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 --------------------------------------------- | ||
| "SNLV27_ElastoDyn.dat" EDFile - Name of file containing ElastoDyn input parameters (quoted string) | ||
| "unused" BDBldFile(1) - Name of file containing BeamDyn input parameters for blade 1 (quoted string) | ||
| "unused" BDBldFile(2) - Name of file containing BeamDyn input parameters for blade 2 (quoted string) | ||
| "unused" BDBldFile(3) - Name of file containing BeamDyn input parameters for blade 3 (quoted string) | ||
| "SNLV27_InflowWind.dat" InflowFile - Name of file containing inflow wind input parameters (quoted string) | ||
| "SNLV27_AeroDyn15OF2.dat" AeroFile - Name of file containing aerodynamic input parameters (quoted string) | ||
| "SNLV27_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 -------------------------------------------------- | ||
| False SumPrint - Print summary data to "<RootName>.sum" (flag) | ||
| 10 SttsTime - Amount of time between screen status messages (s) | ||
| 99999 ChkptTime - Amount of time between creating checkpoint files for potential restart (s) | ||
| 0.005 DT_Out - Time step for tabular output (s) (or "default") | ||
| 0 TStart - Time to begin tabular output (s) | ||
| 2 OutFileFmt - Format for tabular (time-marching) output file (switch) {1: text file [<RootName>.out], 2: binary file [<RootName>.outb], 3: both} | ||
| 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) | ||
| 2 NLinTimes - Number of times to linearize (-) [>=1] [unused if Linearize=False] | ||
| 30.0, 60.0 LinTimes - List of times at which to linearize (s) [1 to NLinTimes] [unused if Linearize=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} | ||
| 2 VTK_type - Type of VTK visualization data: (switch) {1=surfaces; 2=basic meshes (lines/points); 3=all meshes (debug)} [unused if WrVTK=0] | ||
| False 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] |
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