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update scripts to support new aerodyn api
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@ptrbortolotti
ptrbortolotti committed Jan 27, 2021
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72 changes: 36 additions & 36 deletions examples/01_aeroelasticse/OpenFAST_models/BAR_00/OpenFAST_BAR_00_AeroDyn15.dat
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------- AERODYN v15.03.* INPUT FILE ------------------------------------------------
Generated with AeroElasticSE FAST driver
====== 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 AFAeroMod - Type of blade airfoil aerodynamics model (switch) {1=steady model, 2=Beddoes-Leishman unsteady model} [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}
True 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) TRUE will turn off unsteady aerodynamics
False CompAA Flag to compute AeroAcoustics calculation [only used when WakeMod=1 or 2]
"AeroAcousticsInput.dat" AA_InputFile - Aeroacoustics input file
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}
1 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]
"AeroAcousticsInput.dat" AA_InputFile - AeroAcoustics input file [used only when CompAA=true]
====== Environmental Conditions ===================================================================
1.225000000000000e+00 AirDens - Air density (kg/m^3)
1.477551020408163e-05 KinVisc - Kinematic air viscosity (m^2/s)
Expand All @@ -20,23 +20,23 @@ False CompAA Flag to compute AeroAcoustics calculation [on
1.700000000000000e+03 Pvap - Vapour pressure of fluid (Pa) [used only when CavitCheck=True]
5.000000000000000e-01 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]
True AIDrag - Include the drag term in the axial-induction calculation? (flag) [used only when WakeMod=1]
True 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]
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]
True AIDrag - Include the drag term in the axial-induction calculation? (flag) [unused when WakeMod=0 or 3]
True 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=1]
1 DBEMT_Mod - Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2]
20 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=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]
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 (-)
Expand Down Expand Up @@ -80,20 +80,20 @@ True UseBlCm - Include aerodynamic pitching moment in calc
"OpenFAST_BAR_00_AeroDyn15_blade.dat" ADBlFile(1) - Name of file containing distributed aerodynamic properties for Blade #1 (-)
"OpenFAST_BAR_00_AeroDyn15_blade.dat" ADBlFile(2) - Name of file containing distributed aerodynamic properties for Blade #2 (-) [unused if NumBl < 2]
"OpenFAST_BAR_00_AeroDyn15_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]
9 NumTwrNds - Number of tower nodes used in the analysis (-) [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True]
TwrElev TwrDiam TwrCd
(m) (m) (-)
2.740000000000000e+01 6.000000000000000e+00 1.000000000000000e+00
4.110000000000000e+01 6.000000000000000e+00 1.000000000000000e+00
5.480000000000000e+01 6.000000000000000e+00 1.000000000000000e+00
6.850000000000000e+01 6.000000000000000e+00 1.000000000000000e+00
8.220000000000000e+01 6.000000000000000e+00 1.000000000000000e+00
9.590000000000001e+01 6.000000000000000e+00 1.000000000000000e+00
1.096000000000000e+02 6.000000000000000e+00 1.000000000000000e+00
1.233000000000000e+02 5.890792130000000e+00 1.000000000000000e+00
1.370000000000000e+02 5.530325920000000e+00 1.000000000000000e+00
====== Tower Influence and Aerodynamics ============================================================= [used only when TwrPotent/=0, TwrShadow=True, or TwrAero=True]
====== Tower Influence and Aerodynamics ============================================================= [used only when TwrPotent/=0, TwrShadow/=0, or TwrAero=True]
9 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) (-) (-)
2.740000000000000e+01 6.000000000000000e+00 1.000000000000000e+00 1.000000000000000e-01
4.110000000000000e+01 6.000000000000000e+00 1.000000000000000e+00 1.000000000000000e-01
5.480000000000000e+01 6.000000000000000e+00 1.000000000000000e+00 1.000000000000000e-01
6.850000000000000e+01 6.000000000000000e+00 1.000000000000000e+00 1.000000000000000e-01
8.220000000000000e+01 6.000000000000000e+00 1.000000000000000e+00 1.000000000000000e-01
9.590000000000001e+01 6.000000000000000e+00 1.000000000000000e+00 1.000000000000000e-01
1.096000000000000e+02 6.000000000000000e+00 1.000000000000000e+00 1.000000000000000e-01
1.233000000000000e+02 5.890792130000000e+00 1.000000000000000e+00 1.000000000000000e-01
1.370000000000000e+02 5.530325920000000e+00 1.000000000000000e+00 1.000000000000000e-01
====== Outputs ====================================================================================
True SumPrint - Generate a summary file listing input options and interpolated properties to "<rootname>.AD.sum"? (flag)
9 NBlOuts - Number of blade node outputs [0 - 9] (-)
4, 7, 10, 13, 16, 18, 21, 24, 27 BlOutNd - Blade nodes whose values will be output (-)
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