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Update Test_Cases/ for OpenFAST 2.5.0
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@dzalkind
dzalkind committed Feb 2, 2021
1 parent b492424 commit 607d07e
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22 changes: 12 additions & 10 deletions Test_Cases/BAR_10/BAR_10_InflowFile.dat
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Expand Up @@ -2,24 +2,25 @@
Generated with AeroElasticSE FAST driver
---------------------------------------------------------------------------------------------------------------
False Echo - Echo input data to <RootName>.ech (flag)
3 WindType - switch for wind file type (1=steady; 2=uniform; 3=binary TurbSim FF; 4=binary Bladed-style FF; 5=HAWC format; 6=User defined)
1 WindType - switch for wind file type (1=steady; 2=uniform; 3=binary TurbSim FF; 4=binary Bladed-style FF; 5=HAWC format; 6=User defined)
0.0 PropagationDir - Direction of wind propagation (meteoroligical rotation from aligned with X (positive rotates towards -Y) -- degrees)
0 VFlowAng - Upflow angle (degrees) (not used for native Bladed format WindType=7)
1 NWindVel - Number of points to output the wind velocity (0 to 9)
0.0 WindVxiList - List of coordinates in the inertial X direction (m)
0.0 WindVyiList - List of coordinates in the inertial Y direction (m)
90.0 WindVziList - List of coordinates in the inertial Z direction (m)
================== Parameters for Steady Wind Conditions [used only for WindType = 1] =========================
10.0 HWindSpeed - Horizontal windspeed (m/s)
140.0 RefHtT1 - Reference height for horizontal wind speed (m)
0.2 PLexp - Power law exponent (-)
140.0 RefHt - Reference height for horizontal wind speed (m)
0.12 PLexp - Power law exponent (-)
================== Parameters for Uniform wind file [used only for WindType = 2] ============================
"/Users/pbortolo/work/2_openfast/BAR/OpenFAST_Models/BAR_00/Wind/140m_12mps.bts" FilenameT2 - Filename of time series data for uniform wind field. (-)
140.0 RefHtT2 - Reference height for horizontal wind speed (m)
"Wind/NoShr_9-14_Inc1_50s.wnd" Filename_Uni - Filename of time series data for uniform wind field. (-)
140.0 RefHt_Uni - Reference height for horizontal wind speed (m)
125.88 RefLength - Reference length for linear horizontal and vertical sheer (-)
================== Parameters for Binary TurbSim Full-Field files [used only for WindType = 3] ==============
"/Users/nabbas/Documents/WindEnergyToolbox/WindFiles/TurbWind/140m/140m_12mps.bts" FilenameT3 - Name of the Full field wind file to use (.bts)
"Wind/145m_11mps_ClassA1ETM.bts" FileName_BTS - Name of the Full field wind file to use (.bts)
================== Parameters for Binary Bladed-style Full-Field files [used only for WindType = 4] =========
"90m_12mps_twr" FilenameT4 - Rootname of the full-field wind file to use (.wnd, .sum)
"Wind/90m_12mps_twr" FilenameRoot - Rootname of the full-field wind file to use (.wnd, .sum)
False TowerFile - Have tower file (.twr) (flag)
================== Parameters for HAWC-format binary files [Only used with WindType = 5] =====================
"/Users/pbortolo/work/2_openfast/BAR/OpenFAST_Models/BAR_00/basic_5u.bin" FileName_u - name of the file containing the u-component fluctuating wind (.bin)
Expand All @@ -31,7 +32,7 @@ False TowerFile - Have tower file (.twr) (flag)
16.0 dx - distance (in meters) between points in the x direction (m)
3.0 dy - distance (in meters) between points in the y direction (m)
3.0 dz - distance (in meters) between points in the z direction (m)
140.0 RefHtT5 - reference height; the height (in meters) of the vertical center of the grid (m)
140.0 RefHt_Hawc - reference height; the height (in meters) of the vertical center of the grid (m)
------------- Scaling parameters for turbulence ---------------------------------------------------------
2 ScaleMethod - Turbulence scaling method [0 = none, 1 = direct scaling, 2 = calculate scaling factor based on a desired standard deviation]
1.0 SFx - Turbulence scaling factor for the x direction (-) [ScaleMethod=1]
Expand All @@ -43,11 +44,12 @@ False TowerFile - Have tower file (.twr) (flag)
------------- Mean wind profile parameters (added to HAWC-format files) ---------------------------------
12.0 URef - Mean u-component wind speed at the reference height (m/s)
2 WindProfile - Wind profile type (0=constant;1=logarithmic,2=power law)
0.2 PLExp - Power law exponent (-) (used for PL wind profile type only)
0.2 PLExp_Hawc - Power law exponent (-) (used for PL wind profile type only)
0.03 Z0 - Surface roughness length (m) (used for LG wind profile type only)
0 XOffset - Initial offset in +x direction (shift of wind box)
====================== OUTPUT ==================================================
False SumPrint - Print summary data to <RootName>.IfW.sum (flag)
OutList - The next line(s) contains a list of output parameters. See OutListParameters.xlsx for a listing of available output channels, (-)
"Wind1VelX"
Wind1VelX
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
---------------------------------------------------------------------------------------
2 changes: 1 addition & 1 deletion Test_Cases/BAR_10/BAR_10_ServoDyn.dat
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Expand Up @@ -63,7 +63,7 @@ False CompNTMD - Compute nacelle tuned mass damper {true/fal
False CompTTMD - Compute tower tuned mass damper {true/false} (flag)
"b.dat" TTMDfile - Name of the file for tower tuned mass damper (quoted string) [unused when CompTTMD is false]
---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface]
"/Users/nabbas/Documents/WindEnergyToolbox/ROSCO/build/libdiscon.dylib" DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
"../../ROSCO/build/libdiscon.dylib" DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
"BAR_10_DISCON.IN" DLL_InFile - Name of input file sent to the DLL (-) [used only with Bladed Interface]
"DISCON" DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface]
"default" DLL_DT - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface]
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10 changes: 5 additions & 5 deletions Test_Cases/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi_MoorDyn.dat
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Expand Up @@ -18,11 +18,11 @@ Node Type X Y Z M V FX FY FZ CdA CA
6 Fixed 418.800 -725.383 -200.000 0 0 0 0 0 0 0
---------------------- LINE PROPERTIES --------------------------------------
3 NLines - number of line objects
Line LineType UnstrLen NumSegs NodeAnch NodeFair Flags/Outputs
(-) (-) (m) (-) (-) (-) (-)
1 main 850.00 50 2 1 -
2 main 850.00 50 4 3 -
3 main 850.00 50 6 5 -
Line LineType UnstrLen NumSegs NodeAnch NodeFair Flags/Outputs Control
(-) (-) (m) (-) (-) (-) (-) (-)
1 main 850.00 50 2 1 - 0
2 main 850.00 50 4 3 - 0
3 main 850.00 50 6 5 - 0
---------------------- SOLVER OPTIONS ---------------------------------------
0.001 dtM - time step to use in mooring integration (s)
3.0e6 kbot - bottom stiffness (Pa/m)
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2 changes: 1 addition & 1 deletion Test_Cases/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT-UMaineSemi_ServoDyn.dat
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Expand Up @@ -63,7 +63,7 @@ False CompNTMD - Compute nacelle tuned mass damper {true/fal
False CompTTMD - Compute tower tuned mass damper {true/false} (flag)
"unused" TTMDfile - Name of the file for tower tuned mass damper (quoted string) [unused when CompTTMD is false]
---------------------- BLADED INTERFACE ---------------------------------------- [used only with Bladed Interface]
"../../ROSCO/libdiscon.dylib" DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
"../../ROSCO/build/libdiscon.dylib" DLL_FileName - Name/location of the dynamic library {.dll [Windows] or .so [Linux]} in the Bladed-DLL format (-) [used only with Bladed Interface]
"ServoData/DISCON-UMaineSemi.IN" DLL_InFile - Name of input file sent to the DLL (-) [used only with Bladed Interface]
"DISCON" DLL_ProcName - Name of procedure in DLL to be called (-) [case sensitive; used only with DLL Interface]
"default" DLL_DT - Communication interval for dynamic library (s) (or "default") [used only with Bladed Interface]
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37 changes: 20 additions & 17 deletions Test_Cases/IEA-15-240-RWT-UMaineSemi/IEA-15-240-RWT_AeroDyn15.dat
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Expand Up @@ -3,15 +3,15 @@ IEA 15 MW Offshore Reference Turbine
====== 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 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}
False TwrShadow - Calculate tower influence on wind based on downstream tower shadow? (flag)
False 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) 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 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)
1.479232653061225e-05 KinVisc - Kinematic air viscosity (m^2/s)
Expand All @@ -20,23 +20,23 @@ False CompAA - Flag to compute AeroAcoustics calculation [
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]
500 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]
500 MaxIter - Maximum number of iteration steps (-) [unused when WakeMod=0]
====== Dynamic Blade-Element/Momentum Theory Options ====================================================== [used only when WakeMod=1]
2 DBEMT_Mod - Type of dynamic BEMT (DBEMT) model {1=constant tau1, 2=time-dependent tau1} (-) [used only when WakeMod=2]
2 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 @@ -130,6 +130,9 @@ True SumPrint - Generate a summary file listing input optio
"RtAeroMzh"
"RtVAvgxh"
"RtAeroCp"
"RtAeroCt"
"RtArea"
"RtSpeed"
"RtTSR"
END of input file (the word "END" must appear in the first 3 columns of this last OutList line)
---------------------------------------------------------------------------------------
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